WO2017096762A1 - Aircraft control method, mobile terminal and storage medium - Google Patents

Aircraft control method, mobile terminal and storage medium Download PDF

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Publication number
WO2017096762A1
WO2017096762A1 PCT/CN2016/083287 CN2016083287W WO2017096762A1 WO 2017096762 A1 WO2017096762 A1 WO 2017096762A1 CN 2016083287 W CN2016083287 W CN 2016083287W WO 2017096762 A1 WO2017096762 A1 WO 2017096762A1
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WO
WIPO (PCT)
Prior art keywords
aircraft
sensor data
touch
touch operation
sensor
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Application number
PCT/CN2016/083287
Other languages
French (fr)
Chinese (zh)
Inventor
黎凯锋
李家伦
宁京
Original Assignee
腾讯科技(深圳)有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Application filed by 腾讯科技(深圳)有限公司 filed Critical 腾讯科技(深圳)有限公司
Publication of WO2017096762A1 publication Critical patent/WO2017096762A1/en
Priority to US15/957,749 priority Critical patent/US10587790B2/en
Priority to US15/959,014 priority patent/US10863073B2/en
Priority to US15/959,007 priority patent/US10674062B2/en
Priority to US15/959,032 priority patent/US10623621B2/en

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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0011Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement
    • G05D1/0016Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots associated with a remote control arrangement characterised by the operator's input device
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10Simultaneous control of position or course in three dimensions
    • G05D1/101Simultaneous control of position or course in three dimensions specially adapted for aircraft
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/048Interaction techniques based on graphical user interfaces [GUI]
    • G06F3/0487Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser
    • G06F3/0488Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser using a touch-screen or digitiser, e.g. input of commands through traced gestures
    • GPHYSICS
    • G06COMPUTING; CALCULATING OR COUNTING
    • G06FELECTRIC DIGITAL DATA PROCESSING
    • G06F3/00Input arrangements for transferring data to be processed into a form capable of being handled by the computer; Output arrangements for transferring data from processing unit to output unit, e.g. interface arrangements
    • G06F3/01Input arrangements or combined input and output arrangements for interaction between user and computer
    • G06F3/048Interaction techniques based on graphical user interfaces [GUI]
    • G06F3/0487Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser
    • G06F3/0488Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser using a touch-screen or digitiser, e.g. input of commands through traced gestures
    • G06F3/04883Interaction techniques based on graphical user interfaces [GUI] using specific features provided by the input device, e.g. functions controlled by the rotation of a mouse with dual sensing arrangements, or of the nature of the input device, e.g. tap gestures based on pressure sensed by a digitiser using a touch-screen or digitiser, e.g. input of commands through traced gestures for inputting data by handwriting, e.g. gesture or text
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64UUNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U2201/00UAVs characterised by their flight controls
    • B64U2201/20Remote controls

Definitions

  • the present invention relates to the field of aircraft technology, and in particular, to an aircraft control method, a mobile terminal, and a storage medium.
  • UAV Unmanned Aerial Vehicle
  • UAVs include unmanned helicopters, unmanned fixed-wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned paragliders.
  • the drone was originally used in the military field and was mainly used as a reconnaissance aircraft and a drone. With the reduction in the cost of drones, drones have gradually entered the civilian sector.
  • the operation of the drone is mainly realized by the joystick controller, and can also be realized by the mobile terminal simulating the joystick controller.
  • both the joystick controller and the analog joystick controller require the user to have certain basic capabilities to control the drone. It is difficult for new users who have not touched the joystick controller to operate, and the user has no other options. Control method. Therefore, the current drone control method has a single control mode and needs to be improved.
  • an aircraft handling method a mobile terminal, and a storage medium are provided.
  • An aircraft handling method includes:
  • the aircraft maneuver command is sent to the aircraft.
  • a mobile terminal comprising a memory and a processor, the memory storing computer readable instructions, the computer readable instructions being executed by the processor, such that the processor performs the following steps:
  • the aircraft maneuver command is sent to the aircraft.
  • One or more computer readable non-volatile storage media storing computer readable instructions, when executed by one or more processors, cause the one or more processors to perform the steps of:
  • the aircraft maneuver command is sent to the aircraft.
  • FIG 1 is an application environment diagram of an aircraft handling system in an embodiment
  • FIG. 2 is a schematic structural diagram of a mobile terminal applying an aircraft handling method in an embodiment
  • Figure 3 is a schematic structural view of an aircraft in an embodiment
  • FIG. 4 is a schematic flow chart of an aircraft handling method in an embodiment
  • FIG. 5 is a schematic diagram of a display page displayed by a mobile terminal in an embodiment
  • FIG. 6 is a schematic diagram of an aircraft control interface displayed by a mobile terminal in an embodiment
  • FIG. 7 is a schematic flow chart of a step of manipulating an aircraft according to a touch operation on a second touch area in one embodiment
  • Figure 8 is a schematic illustration of an aircraft handling interface in one embodiment
  • FIG. 9 is a flow chart showing the steps of obtaining sensor control commands from sensor data in an embodiment
  • FIG. 10 is a schematic diagram of a gesture in which the user swipes the mobile terminal in four main directions by pressing the first touch area to control the aircraft to perform four actions respectively;
  • FIG. 11 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a first direction in an embodiment
  • FIG. 12 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a second direction in an embodiment
  • FIG. 13 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a third direction in an embodiment
  • FIG. 14 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a fourth direction in an embodiment
  • 15 is a flow chart showing the steps of selecting a preset automatic control mode to operate an aircraft in one embodiment
  • 16 is a structural block diagram of a mobile terminal in an embodiment
  • 17 is a structural block diagram of a mobile terminal in another embodiment
  • FIG. 18 is a structural block diagram of a sensor data processing module in an embodiment
  • Figure 19 is a block diagram showing the structure of a mobile terminal in still another embodiment.
  • an aircraft handling system 100 includes a mobile terminal 102 and an aircraft 104.
  • a wireless connection is established between the mobile terminal 102 and the aircraft 104 by which data is transferred between the mobile terminal 102 and the aircraft 104.
  • the aircraft 104 is a flight device that can be remotely controlled, and may be a drone, and specifically may be any one of a fixed-wing drone, a rotor-wing drone, a wing-wing drone, a flapping drone, and an unmanned airship.
  • the aircraft 104 can also be a powered aviation model.
  • a mobile terminal 102 includes a processor coupled via a system bus, a non-volatile storage medium, an internal memory, a communication device, a display screen, and an input device.
  • the processor has computing functionality and functionality to control operation of the mobile terminal 102, the processor being configured to perform an aircraft handling method.
  • the non-volatile storage medium includes at least one of a magnetic storage medium, an optical storage medium, and a flash storage medium.
  • the non-volatile storage medium stores an operating system.
  • the non-volatile storage medium or internal memory can store computer readable instructions that, when executed by the processor, cause the processor to perform an aircraft manipulation method.
  • the internal memory is used to provide a cache for the operating system and computer readable instructions.
  • the communication device is for wireless communication with the aircraft 104.
  • the display includes at least one of a liquid crystal display, a flexible display, and an electronic ink display.
  • the input device includes at least one of a physical button, a trackball, a touchpad, and a touch layer overlapping the display screen, wherein the touch layer and the display screen are combined to form a touch screen.
  • the mobile terminal 102 may be at least one of a mobile phone, a tablet, a PDA (Personal Digital Assistant), and a touch remote control.
  • an aircraft 104 including a pass system Bus-connected processor, non-volatile storage medium, internal memory, communication device, flight drive, camera, and positioning device.
  • the processor has a computing function and a function to control the operation of the aircraft 104, the processor being configured to execute a manipulation command or a combination manipulation command from the mobile terminal.
  • the non-volatile storage medium includes at least one of a magnetic storage medium, an optical storage medium, and a flash storage medium.
  • the non-volatile storage medium stores an operating system and a manipulation instruction execution device for executing a manipulation command or a combination manipulation command from the mobile terminal.
  • the internal memory is used to provide a cache for the operating system and the manipulation instruction execution device.
  • the communication device is for wirelessly communicating with the mobile terminal 102.
  • the flight drive is used to control the flight behavior of the aircraft of the aircraft 104, primarily by controlling the flight speed and flight direction of the aircraft 104.
  • the flight drive mainly includes rotor and rotor control devices.
  • the camera is used to capture images, including images and videos.
  • the positioning device may be a GPS (Global Positioning System) positioning device for locating the position of the aircraft 104.
  • an aircraft maneuvering method is provided. This embodiment is exemplified by the method applied to the mobile terminal 102 of FIGS. 1 and 2 described above. The method comprises the following steps:
  • Step 402 displaying an aircraft manipulation interface.
  • the mobile terminal runs an aircraft control application
  • the aircraft control application has the function of manipulating the aircraft, and may also have a function of processing photos or videos taken by the aircraft, where the processing of the photos or videos taken by the aircraft mainly includes classification. , show, share with social friends, and generate travel routes.
  • the mobile terminal may specifically sort the travel route according to the shooting time of the photo or video, and may also sort the geographic location information recorded when the photo or video is taken according to the corresponding shooting time to generate a travel route.
  • the travel route here can reflect the travel route of the aircraft, and can further reflect the travel route of the user.
  • the mobile terminal provides an aircraft control interface for triggering aircraft maneuver commands through the aircraft control application, specifically to the aircraft control interface on a display page for displaying photos or videos taken by the aircraft.
  • the mobile terminal runs the aircraft control application, first enters the display page as shown in FIG. 5, and the user can classify and view the photos taken by the aircraft in the display page or The video is shared with social friends, and it can also show the route generated based on the photos or videos taken by the aircraft.
  • the mobile terminal enters the aircraft control interface as shown in FIG. 6 upon detecting the operation of the aircraft control icon 502.
  • Step 404 detecting a touch operation acting on the aircraft control interface.
  • the first touch area is a specific area in the aircraft control interface for supporting the touch operation.
  • the first touch area may be a button, and the button defaults to the first state, and changes to the second state when the touch operation is detected, where the state includes at least one of a shape, a color, and a pattern, for example, the button is convex by default.
  • the up state changes to a sinking state after the touch operation is detected.
  • the first touch area may also be an area identified by a preset mark, such as an area circled by a virtual frame or identified by a special color.
  • the first touch area may also be unmarked, but instead indicated by a guide icon when entering the aircraft control interface for the first time.
  • the touch operation may specifically be a touch click operation, a touch double click operation, a touch long press operation, a sliding operation, and a multi-touch operation
  • the multi-touch operation is based on operations of multiple touch points, such as triggering multiple touch points. After that, multiple touch points are collected, or multiple touch points are triggered, and then multiple touch points are spread.
  • the touch operation is applied to the first touch area, and the touch point of the touch operation is in the first touch area.
  • the mobile terminal can detect the touch operation acting on the aircraft control interface in real time or periodically.
  • the first touch area may be an area 602 located in the aircraft control interface.
  • the mobile terminal may detect the action.
  • a touch body such as a stylus or a user's finger.
  • Step 406 If the touch operation is detected, the sensor data is acquired, and the aircraft manipulation command is obtained according to at least the sensor data.
  • the mobile terminal can specifically read the sensor data from the corresponding sensor through an interface that reads the sensor data, wherein the sensor data can be sensor data of the plurality of sensors.
  • the sensor data is from at least one of a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor.
  • the mobile terminal can obtain an aircraft manipulation command according to the mapping relationship between the sensor data and the aircraft manipulation command, and the acquired sensor data.
  • the mapping relationship between the sensor data and the aircraft maneuver command can be represented by a function, the argument of the function can be sensor data, and the dependent variable can be the identifier of the mapped aircraft maneuver instruction.
  • the aircraft control command may be a control command for controlling the flight state of the aircraft and the attitude of the aircraft, or may be a control command for controlling the aircraft to take a photo or video, or may be other instructions for controlling the aircraft to perform an action.
  • the flight state such as at least one of a flight direction, a flight speed, a flying height, a hover, and a flight destination, the attitude of the aircraft such as a side body or a rotation.
  • the sensor data is a pressure value from a pressure sensor, or a temperature value from a temperature sensor, or a lightness value from a light sensor
  • an aircraft for controlling the flight speed of the aircraft can be obtained based on the sensor data.
  • Manipulating commands such as the higher the pressure value, the faster the aircraft flies, or the higher the temperature, the faster the aircraft flies.
  • an aircraft control command for decelerating when the distance value is less than the first preset value and stopping when the distance value is less than the second preset value may be obtained according to the sensor data, where the first The preset value is greater than the second preset value.
  • Step 408 transmitting an aircraft manipulation command to the aircraft.
  • the mobile terminal transmits the aircraft manipulation command obtained according to the sensor data to the aircraft through a wireless connection with the aircraft, so that the aircraft performs the action specified by the aircraft manipulation command after receiving the aircraft manipulation command. If the aircraft receives a plurality of aircraft maneuver commands, the actions specified by the respective aircraft maneuver commands may be sequentially executed in the order of reception.
  • the aircraft control method displays an aircraft control interface, and the aircraft control interface has a first touch area.
  • the sensor data is used to generate an aircraft control command and sent to the aircraft.
  • the user can control the aircraft by changing the sensor data detected by the sensor, and provides a simple and brand-new control mode, so that the user is manipulating the aircraft. There are more choices and it is more convenient to control the aircraft.
  • step 406 includes: if the first touch operation for opening the sensor control mode in the first touch area of the aircraft control interface is detected, acquiring sensor data, and obtaining the aircraft based on at least the sensor data. The command is commanded until the second touch operation acting on the first touch area is detected to stop.
  • the touch operation detected by the mobile terminal includes a first touch operation for turning on the sensor control mode and a second touch operation for turning off the sensor control mode.
  • the sensor control mode refers to a mode in which the aircraft is manipulated by sensor data.
  • the mobile terminal acquires sensor data after turning on the sensor control mode and obtains an aircraft control command based on at least the sensor data, and transmits the aircraft control command to the aircraft.
  • the sensor data will no longer be acquired, or the aircraft control command will no longer be obtained according to the sensor data, or the aircraft control command will not be sent to the aircraft, but the aircraft can be manipulated by other means, such as by simulation.
  • the joystick controls the aircraft.
  • the timing of entering the sensor control mode can be flexibly controlled by the touch operation for turning the sensor control mode on and off, respectively, thereby using the change of the sensor data detected by the sensor to control the aircraft in the sensor control mode.
  • the handling of the aircraft is more convenient.
  • the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be the same.
  • the touch operation can be selected from a touch click operation, a touch double click operation, a slide operation, and a multi-touch operation.
  • the sensor control mode is turned on, and the sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the aircraft control command is sent to the aircraft. If a touch click operation on the first touch area is detected again, the sensor control mode is turned off.
  • the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be different.
  • the two touch operations can be selected from a touch click operation, a touch double click operation, a slide operation, and a multi-touch operation, respectively.
  • the sensor control mode is turned on, and sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the flight is performed.
  • the aircraft sends an aircraft control command. If a touch double click operation on the first touch area is detected, the sensor control mode is turned off.
  • the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be included in one combined touch operation.
  • the combined touch operation such as a touch long press operation, includes a touch operation that triggers a long press operation and a touch operation that releases a long press operation.
  • the step 406 includes: starting from the detection of the third touch operation, and if the timing reaches the preset duration and the third touch operation remains applied to the first touch area in the aircraft control interface, acquiring The sensor data, and at least the aircraft control command is obtained according to the sensor data until the third touch operation is stopped.
  • the third touch operation detected in the embodiment is a continuous touch operation
  • the mobile terminal detects the third touch operation after the third touch operation is used for the first touch area.
  • the action time of the touch operation refers to a time period from when the touch operation is detected to when the touch operation disappears.
  • the preset duration is for distinguishing from the touch operation. If the touch point disappears within the preset duration from the detection of the touch point, the touch operation is recognized as a touch operation, and the touch point does not disappear if the preset time is reached. , it is recognized as a continuous touch operation that needs to be detected, and enters the sensor control mode.
  • the first touch operation for turning on the sensor control mode is started when the touch point of the third touch operation is detected and the time is up to the preset time. The effect of the touch point on the first touch area disappears.
  • the time is started. If the touch time is still applied to the first touch area when the preset time is reached, the aircraft may be prevented from being out of control due to the user accidentally touching the first touch area.
  • the mobile terminal may also acquire sensor data immediately after detecting the touch operation, and at least obtain an aircraft control command according to the sensor data, and send an aircraft control command to the aircraft until the touch point is opposite to the first touch area. The role disappears.
  • the method further includes the step of manipulating the aircraft according to the touch operation on the second touch area, and specifically includes the following steps:
  • Step 702 detecting a touch operation applied to the second touch area in the aircraft control interface; the second touch area is used to simulate the joystick operation.
  • the second touch area is a specific area in the aircraft manipulation interface for withstanding a touch operation to simulate a joystick operation.
  • Touch operations such as touch click operations, touch double tap operations, touch long press operations, swipe operations, and multi-touch operations.
  • the touch operation applied to the second touch area and the touch operation applied to the first touch area respectively implement different control modes.
  • the second touch area can surround the first touch area.
  • the second touch area does not overlap with the first touch area.
  • the touch operation and the detected touch operation may be the same. In other embodiments, the second touch area can be separated from the first touch area.
  • Step 704 Acquire an analog joystick manipulation command triggered by the touch operation.
  • step 706 an analog joystick manipulation command is sent to the aircraft.
  • the touch operation acts on different regions of the second touch area, and different analog joystick manipulation commands can be triggered respectively.
  • the specific second touch area can define four main directions, such as up, down, left and right, so that the mobile terminal can trigger the corresponding analog joystick control according to the relative position of the second touch area relative to the four main directions according to the touch operation. instruction.
  • the analog joystick control command does not conflict with the aircraft control command.
  • the analog rocker steering command is used to manipulate the vertical movement of the aircraft and the change in attitude of the aircraft, and the aircraft maneuver command is used to manipulate the movement of the aircraft in various directions along the horizontal plane.
  • the mobile terminal may trigger the touch operation.
  • the aircraft After the analog joystick manipulation command corresponding to the main direction is sent to the aircraft, the aircraft can perform the ascending, descending, left-handed or right-handed motion according to the received analog joystick manipulation command.
  • the mobile terminal may trigger the corresponding combined analog joystick manipulation command according to the component of the touch operation mapped by the touch point in the main direction, and combine The analog joystick manipulation command is sent to the aircraft, and the aircraft can be received according to the The combined analog joystick manipulation command performs a left-handed rise, a right-handed rise, a left-handed fall, or a right-handed down action.
  • the mobile terminal detects a touch operation applied to the aircraft control interface, and detects a touch operation of the second touch area acting on the aircraft control interface, thereby implementing different operations of the aircraft according to a combination of different detection results. the way. This makes the aircraft's control mode more diverse, and the handling of the aircraft is more flexible and convenient.
  • step 406 includes: if it is detected that the touch point of the fourth touch operation acts on the first touch area, acquiring sensor data, and at least obtaining an aircraft control command according to the sensor data until the touch point disappears Stop when.
  • the method further includes: when the touch point moves to the second touch area in the aircraft control interface, triggering the analog joystick manipulation command according to the position of the touch point in the second touch area and transmitting to the aircraft; the second touch The control area is used to simulate the joystick operation.
  • the fourth touch operation detected in the embodiment is a continuous touch operation, and after detecting the fourth touch operation, the mobile terminal acquires sensor data during the action time of the corresponding touch point, and at least The aircraft control command is obtained based on the sensor data, and the aircraft control command is sent to the aircraft until the touch point disappears.
  • the touch point that detects the fourth touch operation acts on the first touch area, and is the first touch operation for turning on the sensor control mode, and the touch point disappears is the second method for turning off the sensor control mode. Touch operation.
  • the mobile terminal can also start timing when the touch point of the fourth touch operation is detected. If the time reaches the preset time and the corresponding touch point remains in the first touch area, the sensor data is acquired, and at least according to the sensor. The data is obtained by the aircraft control command until the touch point disappears.
  • the first touch operation for turning on the sensor control mode is started when the touch point of the fourth touch operation is detected and the timing is reached, and the touch point disappears to close the sensor control mode.
  • the second touch operation is started when the touch point of the fourth touch operation is detected and the timing is reached.
  • the steps 702 to 706 can be triggered, and the action of the touch point on the second touch area acts on the second touch.
  • the touch operation of the area can be triggered, and the action of the touch point on the second touch area acts on the second touch.
  • the continuous sensor touch control can be sequentially triggered by the fourth touch operation.
  • the mode and the analog joystick control aircraft can realize the one-handed operation of the aircraft, making the operation of the aircraft more convenient and faster.
  • step 406 includes: detecting a touch touch operation of a touch button applied to the second touch area of the aircraft control interface, and detecting sensor data when detecting; detecting the touch button following the touch operation at the second
  • the movement in the touch area or the aircraft control interface acquires an analog joystick manipulation command according to the movement; the aircraft manipulation command is obtained according to the sensor data and the analog joystick manipulation command.
  • the analog joystick control command is a control command of the analog joystick remote control, and specifically defines four main directions in the second touch area, such as up, down, left, and right, so that the touch operation can be applied to the second touch area according to the pressing touch operation.
  • the corresponding analog joystick manipulation command is triggered relative to the relative positions of the four main directions.
  • the analog joystick control command does not conflict with the aircraft control command.
  • the analog rocker steering command is used to manipulate the vertical movement of the aircraft and the change in attitude of the aircraft.
  • the sensor control mode and the analog joystick control aircraft can be successively triggered, and the aircraft can be operated by one hand, so that the operation of the aircraft is more convenient and faster.
  • the step of obtaining an aircraft manipulation command based on at least the sensor data specifically includes the following steps:
  • Step 902 Determine an initial state of the mobile terminal where the sensor is located according to the obtained initial sensor data.
  • the sensor data includes data for reflecting at least one of a posture and a motion of the mobile terminal.
  • the initial sensor data is the sensor data initially received by the mobile terminal after entering the sensor control mode, and is used to determine the current state of the mobile terminal, which is defined as an initial state.
  • the initial state includes an attitude state and a motion state of the mobile terminal, wherein the posture state includes a tilted portion of the mobile terminal, a tilted direction, and a tilt angle, and the like, and the motion state includes a motion speed, a motion acceleration, and a motion direction.
  • the mobile terminal can determine the initial state of the mobile terminal in three-dimensional space according to the three-dimensional fixed reference coordinate system of the mobile terminal.
  • the fixed reference coordinate system is a three-dimensional reference coordinate system, including Straight three axes, where the two axes can be parallel to the display of the mobile terminal, while the remaining one axis is perpendicular to the display.
  • the motion parameters include at least one of a moving direction, a moving range, and a moving speed.
  • Step 904 Determine a subsequent state of the mobile terminal according to the acquired sensor data of the initial sensor data.
  • the mobile terminal continues to acquire subsequent sensor data, thereby determining a subsequent state of the mobile terminal according to the subsequent sensor data, where the subsequent state includes a posture state and a motion state of the mobile terminal, where the posture state includes the mobile terminal tilting
  • the state of motion includes the speed of motion, the acceleration of motion, and the direction of motion.
  • Step 906 generating an aircraft manipulation command according to a change of the subsequent state with respect to the initial state.
  • the mobile terminal compares the subsequent state with the initial state based on the initial state, thereby generating an aircraft manipulation command according to the amount that the subsequent state changes with respect to the initial state. For example, if the initial state of the mobile terminal is inclined by 15° in the lower left corner of the mobile terminal, if the subsequent state is that the lower left corner of the mobile terminal changes from the tilt 15° to the horizontal level, then the lower left corner of the mobile terminal moves in the opposite direction by 15°, and the mobile terminal is at this time. An aircraft maneuver command is generated based on the amount of change.
  • the mobile terminal determines that the initial state of the mobile terminal where the sensor is located is a horizontal state, then the mobile terminal is swung to the left, then the mobile terminal can follow the follow-up
  • the sensor data determines a subsequent state of the mobile terminal, and detects that the mobile terminal moves in a direction along the left side of the screen according to a change in the subsequent state with respect to the initial state.
  • the aircraft control command generated by the mobile terminal is transmitted to the aircraft, the aircraft performs a corresponding action, such as performing a left shifting action, so that the aircraft is linked according to the motion of the mobile terminal.
  • the mobile terminal can detect that the mobile terminal moves along the back side, the upper side, or the next direction of the screen. After the corresponding aircraft maneuver command is sent to the aircraft, the aircraft is caused to perform a right shifting, advancing or retreating action, respectively.
  • the user can pass the first touch area in the arbitrary state of the mobile terminal.
  • the touch operation is used to turn on the sensor control mode, and the mobile terminal initializes, determines an initial state according to the initial sensor data, and then determines a subsequent state according to the subsequent sensor data, and generates an aircraft manipulation command according to the change of the subsequent state with respect to the initial state.
  • the user does not have to place the mobile terminal horizontally to control the aircraft, and the control is more convenient and precise.
  • the mobile terminal when determining the motion state of the mobile terminal, determines whether the motion amplitude exceeds a preset threshold, and if yes, performs step 906; if not, abandoning step 906.
  • the user can swipe the mobile terminal in one direction and slowly return to the mobile terminal in the same direction, so that the mobile terminal can continuously move the motion parameters in the same direction, so that the aircraft can be continuously operated to perform the same operation. Actions.
  • the aircraft control method further includes the step of selecting a preset automatic control mode to operate the aircraft, and specifically includes the following steps:
  • Step 1502 Detect a selection instruction for a preset automatic control mode icon in the aircraft control interface.
  • the mobile terminal can display a plurality of preset automatic manipulation mode icons in the aircraft manipulation interface, such as icons 606, 608, and 610 in FIG.
  • the preset automatic control mode is an automatic control method that uses predefined parameters to control the aircraft to implement predefined actions.
  • Step 1504 Determine a corresponding preset automatic control mode according to the selection instruction.
  • the mobile terminal selects a preset automatic control mode corresponding to the preset automatic control mode icon corresponding to the instruction as a corresponding preset automatic control mode determined according to the selection instruction.
  • Step 1506 reading the determined aircraft combination manipulation command associated with the determined preset automatic control mode.
  • Step 1508 transmitting an aircraft combination manipulation command to the aircraft, so that the aircraft sequentially performs a corresponding series of actions according to the aircraft combination manipulation command.
  • each preset automatic control mode stored on the mobile terminal is pre-associated with a corresponding aircraft combination control command, and after the mobile terminal reads the aircraft combined control command and sends the command to the aircraft, the aircraft sequentially executes according to the aircraft combination control command.
  • the preset automatic control mode includes an in-situ landing mode, and returns to a preset location. At least one of a landing mode, an in-flight emergency hover mode, and a follow-lock target flight mode.
  • the aircraft can automatically complete the in-situ landing after automatically stopping the horizontal movement, gradually reducing the flying height, and stopping the rotor after reaching a ground level. Flight mission.
  • the aircraft may automatically perform the steps of acquiring the preset location coordinates, flying to the preset location coordinates, stopping the horizontal direction, gradually reducing the flight altitude, and arriving at the place. After the plane stops the series of actions of the rotor, the automatic flight task returns to the preset position and falls.
  • the aircraft may complete the automatic flight hovering emergency flight task after automatically performing a series of actions of stopping the horizontal direction movement and maintaining the flight altitude.
  • the aircraft may complete the follow-lock target flight after automatically performing the acquisition of the locked target, the flight to the target preset distance of the distance lock and maintaining a series of actions. Automatic flight mission.
  • the user can quickly control the aircraft by preset the automatic control mode, so that the aircraft automatically completes the corresponding flight task, thereby improving the convenience of operation.
  • the in-situ landing mode, the returning preset landing mode and the flight emergency hover mode can realize emergency hedging or aircraft recovery.
  • the aircraft can be locked automatically after the target is locked, and one user can simultaneously Manipulate multiple aircraft.
  • a mobile terminal 1600 is provided.
  • the internal structure of the mobile terminal 1600 may correspond to the mobile terminal structure as shown in FIG. 2.
  • Each of the following modules may pass all or part of the software. , hardware or a combination thereof.
  • the mobile terminal 1600 includes an interface display module 1601, a touch operation detection module 1602, a sensor data processing module 1603, and a manipulation command transmission module 1604.
  • the interface display module 1601 is configured to display an aircraft manipulation interface.
  • the mobile terminal runs an aircraft control application
  • the aircraft control application has the function of manipulating the aircraft, and may also have a function of processing photos or videos taken by the aircraft.
  • the processing of photos or videos taken by the aircraft here mainly includes classification, display, sharing with social friends, and generating a route of travel.
  • the mobile terminal may specifically sort the travel route according to the shooting time of the photo or video, and may also sort the geographic location information recorded when the photo or video is taken according to the corresponding shooting time to generate a travel route.
  • the travel route here can reflect the travel route of the aircraft, and can further reflect the travel route of the user.
  • the interface display module 1601 provides an aircraft control interface for triggering aircraft maneuver instructions through the aircraft control application, specifically to the aircraft control interface on a display page for displaying photos or videos taken by the aircraft.
  • the mobile terminal runs the aircraft control application, first enters the display page as shown in FIG. 5, in which the user can classify and view the photos or videos taken by the aircraft and share them with social friends, and can also display photos taken according to the aircraft. Or the route generated by the video.
  • the mobile terminal enters the aircraft control interface as shown in FIG. 6 upon detecting the operation of the aircraft control icon 502.
  • the touch operation detecting module 1602 is configured to detect a touch operation applied to the aircraft control interface.
  • the first touch area is a specific area in the aircraft control interface for supporting the touch operation.
  • the first touch area may be a button, and the button defaults to a first state, and changes to a second state when the touch operation detecting module 1602 detects the touch operation, where the state includes at least one of a shape, a color, and a pattern.
  • the button is in a raised state by default, and changes to a sinking state after the touch operation detecting module 1602 detects the touch operation.
  • the first touch area may also be an area identified by a preset mark, such as an area circled by a virtual frame or identified by a special color.
  • the first touch area may also be unmarked, but instead indicated by a guide icon when entering the aircraft control interface for the first time.
  • the touch operation may specifically be a touch click operation, a touch double click operation, a touch long press operation, a sliding operation, and a multi-touch operation
  • the multi-touch operation is based on operations of multiple touch points, such as triggering multiple touch points. After that, multiple touch points are collected, or multiple touch points are triggered, and then multiple touch points are spread.
  • the touch operation is applied to the first touch area, and the touch point of the touch operation is in the first touch area.
  • the touch operation detecting module 1602 can detect the touch operation acting on the aircraft control interface in real time or periodically.
  • the first touch area may be an area located in the aircraft control interface.
  • the user touches the first touch area 602 through the touch body and keeps the touch point from disappearing, and the mobile terminal detects the touch operation on the first touch area 602.
  • a touch body such as a stylus or a user's finger.
  • the sensor data processing module 1603 is configured to acquire sensor data if a touch operation is detected, and obtain an aircraft manipulation command based on at least the sensor data.
  • the sensor data processing module 1603 can specifically read the sensor data from the corresponding sensor through an interface that reads the sensor data, wherein the sensor data can be sensor data of the plurality of sensors.
  • the sensor data is from at least one of a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor.
  • the sensor data processing module 1603 can obtain an aircraft manipulation command according to the mapping relationship between the sensor data and the aircraft manipulation command, and the acquired sensor data.
  • the mapping relationship between the sensor data and the aircraft maneuver command can be represented by a function, the argument of the function can be sensor data, and the dependent variable can be the identifier of the mapped aircraft maneuver instruction.
  • the aircraft control command may be a control command for controlling the flight state of the aircraft and the attitude of the aircraft, or may be a control command for controlling the aircraft to take a photo or video, or may be other instructions for controlling the aircraft to perform an action.
  • the flight state such as at least one of a flight direction, a flight speed, a flying height, a hover, and a flight destination, the attitude of the aircraft such as a side body or a rotation.
  • the sensor data is a pressure value from a pressure sensor, or a temperature value from a temperature sensor, or a lightness value from a light sensor
  • an aircraft for controlling the flight speed of the aircraft can be obtained based on the sensor data.
  • Manipulating commands such as the higher the pressure value, the faster the aircraft flies, or the higher the temperature, the faster the aircraft flies.
  • an aircraft control command for decelerating when the distance value is less than the first preset value and stopping when the distance value is less than the second preset value may be obtained according to the sensor data, where the first The preset value is greater than the second preset value.
  • the command transmission module 1604 is configured to send an aircraft control command to the aircraft.
  • the manipulation command transmitting module 1604 transmits the obtained aircraft manipulation command to the aircraft through a wireless connection with the aircraft, so that the aircraft performs the action specified by the aircraft manipulation command after receiving the aircraft manipulation command. If the aircraft receives a plurality of aircraft maneuver commands, the actions specified by the respective aircraft maneuver commands may be sequentially executed in the order of reception.
  • the mobile terminal 1600 displays an aircraft control interface.
  • the aircraft control interface has a first touch area.
  • the sensor data is used to generate an aircraft control command and sent to the aircraft.
  • the user can control the aircraft by changing the sensor data detected by the sensor, and provides a simple and brand-new control mode, so that the user is manipulating the aircraft. There are more choices and it is more convenient to control the aircraft.
  • the sensor data processing module 1603 is specifically configured to acquire sensor data when detecting a first touch operation for opening the sensor control mode in the first touch area of the aircraft control interface, and at least according to The sensor data is obtained by the aircraft control command until the second touch operation acting on the first touch area is detected.
  • the touch operation detected by the sensor data processing module 1603 includes a first touch operation for turning on the sensor control mode and a second touch operation for turning off the sensor control mode.
  • the sensor control mode refers to a mode in which the aircraft is manipulated by sensor data.
  • the sensor data processing module 1603 acquires sensor data after turning on the sensor control mode and obtains an aircraft control command based on at least the sensor data, and transmits the aircraft control command to the aircraft.
  • the sensor data processing module 1603 will no longer acquire the sensor data after the sensor control mode is turned off, or no longer at least obtain the aircraft control command according to the sensor data, or no longer send the aircraft control command to the aircraft, but can manipulate the aircraft by other means.
  • the aircraft is controlled by an analog joystick.
  • the timing of entering the sensor control mode can be flexibly controlled by the touch operation for turning the sensor control mode on and off, respectively, thereby using the change of the sensor data detected by the sensor to control the aircraft in the sensor control mode.
  • the handling of the aircraft is more convenient.
  • the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be the same.
  • the touch operation can be performed from a touch click operation, Touch double-click, slide, and multi-touch to select.
  • the sensor control mode is turned on, and the sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the aircraft control command is sent to the aircraft. If a touch click operation on the first touch area is detected again, the sensor control mode is turned off.
  • the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be different.
  • the two touch operations can be selected from a touch click operation, a touch double click operation, a slide operation, and a multi-touch operation, respectively.
  • the sensor control mode is turned on, and sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the aircraft control command is sent to the aircraft. If a touch double click operation on the first touch area is detected, the sensor control mode is turned off.
  • the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be included in one combined touch operation.
  • the combined touch operation such as a touch long press operation, includes a touch operation that triggers a long press operation and a touch operation that releases a long press operation.
  • the sensor data processing module 1603 is specifically configured to start timing when the third touch operation is detected, if the timing reaches a preset duration and the third touch operation remains to act on the first touch in the aircraft control interface. For the area, the sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data until the third touch operation is stopped.
  • the touch operation detected in the embodiment is a continuous touch operation
  • the sensor data processing module 1603 acquires a sensor during the use time of the touch operation on the first touch area. Data, and at least according to the sensor data, obtain an aircraft control command, and send an aircraft control command to the aircraft until the effect of the touch point on the first touch area disappears.
  • the action time of the touch operation refers to a time period from when the touch operation is detected to when the touch operation disappears.
  • the preset duration is for distinguishing from the touch operation, and the preset duration from the touch point is detected. After the touch point disappears, it is recognized as a touch operation. If the touch point has not disappeared after reaching the preset time, it is recognized as a continuous touch operation that needs to be detected, and enters the sensor control mode.
  • the first touch operation for turning on the sensor control mode is started when the touch point of the third touch operation is detected and the time is up to the preset time. The effect of the touch point on the first touch area disappears.
  • the time is started. If the touch time is still applied to the first touch area when the preset time is reached, the aircraft may be prevented from being out of control due to the user accidentally touching the first touch area.
  • the sensor data processing module 1603 may also acquire sensor data immediately after detecting the touch operation, and at least obtain an aircraft manipulation command according to the sensor data until the effect of the touch point on the first touch area disappears.
  • the sensor data processing module 1603 is specifically configured to detect a touch touch operation of a touch button applied to the second touch area of the aircraft control interface. When detected, the sensor data is acquired; and the touch button is detected to follow the touch touch. The operation is operated in the second touch area or the aircraft control interface, and the analog joystick manipulation command is acquired according to the movement; the aircraft manipulation command is obtained according to the sensor data and the analog joystick manipulation command.
  • the mobile terminal 1600 further includes a touch operation detection module 1605, an analog joystick manipulation command acquisition module 1606, and an analog joystick manipulation command transmission module 1607.
  • the touch operation detecting module 1605 is configured to detect a touch operation applied to the second touch area in the aircraft control interface.
  • the second touch area is used to simulate the joystick operation.
  • the second touch area is a specific area in the aircraft manipulation interface for withstanding a touch operation to simulate a joystick operation.
  • Touch operations such as touch click operations, touch double tap operations, touch long press operations, swipe operations, and multi-touch operations.
  • the touch operation applied to the second touch area and the touch operation applied to the first touch area respectively implement different control modes.
  • the second touch area can surround the first touch area.
  • the second touch area does not overlap with the first touch area.
  • the touch operation and the detected touch operation may be the same. In other embodiments, the second touch area can be separated from the first touch area.
  • the analog joystick manipulation command acquisition module 1606 is configured to acquire an analog joystick manipulation command triggered by the touch operation.
  • the analog joystick manipulation command sending module 1607 is configured to send an analog joystick manipulation command to the aircraft.
  • the touch operation acts on different regions of the second touch area, and different analog joystick manipulation commands can be triggered respectively.
  • Four main directions may be defined in the second touch area, such as up, down, left and right, so that the analog rocker manipulation command acquisition module 1606 can be triggered according to the relative position of the second touch region relative to the four main directions according to the touch operation.
  • the corresponding analog joystick control command does not conflict with the aircraft control command.
  • the analog rocker steering command is used to manipulate the vertical movement of the aircraft and the change in attitude of the aircraft, and the aircraft maneuver command is used to manipulate the movement of the aircraft in various directions along the horizontal plane.
  • the mobile terminal may trigger the touch operation.
  • the aircraft After the analog joystick manipulation command corresponding to the main direction is sent to the aircraft, the aircraft can perform the ascending, descending, left-handed or right-handed motion according to the received analog joystick manipulation command.
  • the analog joystick manipulation instruction acquisition module 1606 can trigger the corresponding combined analog shake according to the component of the touch operation map of the touch operation in the main direction.
  • the lever manipulation command, the analog joystick manipulation command sending module 1607 sends the combined analog joystick manipulation command to the aircraft, and the aircraft can perform a left-handed rise, a right-handed rise, a left-handed fall, or a right-handed according to the received combined analog joystick manipulation command. The action of falling.
  • the touch operation applied to the control interface of the aircraft is detected, and the touch operation of the second touch area acting on the control interface of the aircraft is detected, so that different control modes of the aircraft are implemented according to a combination of different detection results.
  • the sensor data processing module 1603 is specifically configured to: if the touch point of the fourth touch operation is detected to act on the first touch area, acquire sensor data, and obtain an aircraft control command according to at least the sensor data; Stopping when the touch point disappears; the mobile terminal 1600 also includes shaking
  • the lever control simulation module (not shown) is configured to trigger the analog joystick control according to the position of the touch point in the second touch area when the touch point moves to the second touch area in the aircraft control interface The command is sent to the aircraft; the second touch area is used to simulate the joystick operation.
  • the joystick manipulation simulation module may include the above-described touch operation detection module 1605, an analog joystick manipulation instruction acquisition module 1606, and an analog joystick manipulation command transmission module 1607.
  • the sensor data processing module 1603 includes an initial state determination module 1603a, a subsequent state determination module 1603b, and an aircraft manipulation command generation module 1603c.
  • the initial state determining module 1603a is configured to determine an initial state of the mobile terminal where the sensor is located according to the obtained initial sensor data.
  • the sensor data includes data for reflecting at least one of a posture and a motion of the mobile terminal.
  • the initial sensor data is the sensor data initially received by the mobile terminal after entering the sensor control mode, and is used to determine the current state of the mobile terminal, which is defined as an initial state.
  • the initial state includes an attitude state and a motion state of the mobile terminal, wherein the posture state includes a tilted portion of the mobile terminal, a tilted direction, and a tilt angle, and the like, and the motion state includes a motion speed, a motion acceleration, and a motion direction.
  • the initial state determination module 1603a may determine an initial state of the mobile terminal in three-dimensional space according to a three-dimensional fixed reference coordinate system of the mobile terminal.
  • the fixed reference coordinate system is a three-dimensional reference coordinate system, including three axes perpendicular to each other, two axes may be parallel to the display screen of the mobile terminal, and the remaining one axis is perpendicular to the display screen.
  • the motion parameters include at least one of a moving direction, a moving range, and a moving speed.
  • the subsequent state determining module 1603b is configured to determine a subsequent state of the mobile terminal according to the acquired sensor data subsequent to the sensor data.
  • the subsequent state determining module 1603b continues to acquire subsequent sensor data, thereby determining a subsequent state of the mobile terminal according to the subsequent sensor data, where the subsequent state includes a posture state and a motion state of the mobile terminal, where the posture state includes Mobile terminal tilt
  • the state of motion includes the speed of motion, the acceleration of motion, and the direction of motion.
  • the aircraft maneuver instruction generation module 1603c is configured to generate an aircraft maneuver instruction according to a change of the subsequent state with respect to the initial state.
  • the aircraft manipulation command generation module 1603c compares the subsequent state with the initial state based on the initial state, thereby generating an aircraft manipulation command according to the amount of change of the subsequent state with respect to the initial state. For example, if the initial state of the mobile terminal is inclined by 15° in the lower left corner of the mobile terminal, if the subsequent state is that the lower left corner of the mobile terminal changes from the tilt 15° to the horizontal level, then the lower left corner of the mobile terminal moves in the opposite direction by 15°, and the mobile terminal is at this time. An aircraft maneuver command is generated based on the amount of change.
  • the user can turn on the sensor control mode by using the touch operation on the first touch area in the arbitrary state of the mobile terminal, and the mobile terminal initializes the initial state according to the initial sensor data, and then according to the subsequent The sensor data determines a subsequent state, and an aircraft maneuver command is generated based on a change in the subsequent state relative to the initial state. In this way, the user does not have to place the mobile terminal horizontally to control the aircraft, and the control is more convenient and precise.
  • the sensor data is from at least one of a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor.
  • the mobile terminal 1600 further includes: a preset automatic steering mode determining module 1608, an aircraft combination steering command reading module 1609, and an aircraft combination steering command transmitting module 1610.
  • the preset automatic control mode determining module 1608 is configured to detect a selection instruction for the preset automatic control mode icon in the aircraft control interface; and determine a corresponding preset automatic control mode according to the selection instruction.
  • the preset automatic manipulation mode determination module 1608 can display a plurality of preset automatic manipulation mode icons in the aircraft manipulation interface, such as icons 606, 608, and 610 in FIG. When the user clicks on an icon, the corresponding selection instruction is triggered.
  • the preset automatic control mode is an automatic control method that uses predefined parameters to control the aircraft to implement predefined actions.
  • the preset corresponding to the selection instruction will be
  • the preset automatic control mode corresponding to the motion control mode icon is used as a corresponding preset automatic control mode determined according to the selection instruction.
  • the aircraft combination manipulation command reading module 1609 is configured to read the aircraft combination manipulation command associated with the determined preset automatic control mode.
  • the aircraft combination command transmission module 1610 is configured to send an aircraft combination manipulation command to the aircraft, so that the aircraft sequentially performs a corresponding series of actions according to the aircraft combination manipulation command.
  • each preset automatic control mode stored on the mobile terminal is pre-associated with a corresponding aircraft combination manipulation command, and the aircraft combination manipulation command reading module 1609 reads the aircraft combination manipulation command and is transmitted by the aircraft combination manipulation command transmission module 1610. After the aircraft, the aircraft will perform a series of actions according to the aircraft combination control command to control the aircraft to automatically change from the current state to the target state specified by the preset automatic control mode.
  • the preset automatic control mode includes at least one of an in situ landing mode, a return preset landing mode, an in-flight emergency hover mode, and a follow-lock target flight mode.
  • the aircraft can automatically complete the in-situ landing after automatically stopping the horizontal movement, gradually reducing the flying height, and stopping the rotor after reaching a ground level. Flight mission.
  • the aircraft may automatically perform the steps of acquiring the preset location coordinates, flying to the preset location coordinates, stopping the horizontal direction, gradually reducing the flight altitude, and arriving at the place. After the plane stops the series of actions of the rotor, the automatic flight task returns to the preset position and falls.
  • the aircraft may complete the automatic flight hovering emergency flight task after automatically performing a series of actions of stopping the horizontal direction movement and maintaining the flight altitude.
  • the aircraft may complete the follow-lock target flight after automatically performing the acquisition of the locked target, the flight to the target preset distance of the distance lock and maintaining a series of actions. Automatic flight mission.
  • the user can quickly control the aircraft by using a preset automatic control mode to make the fly The line automatically completes the corresponding flight task, which improves the convenience of operation.
  • the in-situ landing mode, the returning preset landing mode and the flight emergency hover mode can realize emergency hedging or aircraft recovery.
  • the aircraft can be locked automatically after the target is locked, and one user can simultaneously Manipulate multiple aircraft.
  • the storage medium may be a non-volatile storage medium such as a magnetic disk, an optical disk, a read-only memory (ROM), or a random access memory (RAM).

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Abstract

An aircraft control method, comprising: displaying an aircraft control interface; detecting a touch operation that acts on the aircraft control interface; if the touch operation is detected, obtaining sensor data and obtaining an aircraft control instruction at least according to the sensor data; and sending the aircraft control instruction to an aircraft.

Description

飞行器操控方法、移动终端和存储介质Aircraft control method, mobile terminal and storage medium
本申请要求于2015年12月10日提交中国专利局,申请号为201510919245.9,发明名称为“飞行器操控方法和装置”的中国专利申请的优先权,其全部内容通过引用结合在本申请中。The present application claims priority to Chinese Patent Application No. 2015-1091924, filed on Dec. 10, 2015, the entire disclosure of which is incorporated herein by reference.
技术领域Technical field
本发明涉及飞行器技术领域,特别是涉及一种飞行器操控方法、移动终端和存储介质。The present invention relates to the field of aircraft technology, and in particular, to an aircraft control method, a mobile terminal, and a storage medium.
背景技术Background technique
无人驾驶飞机简称“无人机”,英文缩写为“UAV”(Unmanned Aerial Vehicle),是一种远程操纵的不载人飞机。无人机包括无人直升机、无人固定翼机、无人多旋翼飞行器、无人飞艇以及无人伞翼机等。无人机最初应用在军用领域,主要用作侦察机和靶机。随着无人机造价降低,无人机逐渐进入民用领域。The drone is referred to as the "UAV", abbreviated as "UAV" (Unmanned Aerial Vehicle), which is a remotely manned unmanned aircraft. UAVs include unmanned helicopters, unmanned fixed-wing aircraft, unmanned multi-rotor aircraft, unmanned airships, and unmanned paragliders. The drone was originally used in the military field and was mainly used as a reconnaissance aircraft and a drone. With the reduction in the cost of drones, drones have gradually entered the civilian sector.
目前,对无人机进行操控主要通过摇杆控制器来实现,也可以通过移动终端模拟摇杆控制器来实现。然而,无论是摇杆控制器还是模拟摇杆控制器都需要用户具备一定的操控无人机的基础能力,未接触过摇杆控制器的新用户操控存在困难,而用户也没有其它可选的操控方式。因此,目前的无人机操控方法操控方式单一,需要改进。At present, the operation of the drone is mainly realized by the joystick controller, and can also be realized by the mobile terminal simulating the joystick controller. However, both the joystick controller and the analog joystick controller require the user to have certain basic capabilities to control the drone. It is difficult for new users who have not touched the joystick controller to operate, and the user has no other options. Control method. Therefore, the current drone control method has a single control mode and needs to be improved.
发明内容Summary of the invention
根据本申请的各种实施例,提供一种飞行器操控方法、移动终端和存储介质。According to various embodiments of the present application, an aircraft handling method, a mobile terminal, and a storage medium are provided.
一种飞行器操控方法,包括: An aircraft handling method includes:
显示飞行器操控界面;Display the aircraft control interface;
检测作用于所述飞行器操控界面的触控操作;Detecting a touch operation acting on the aircraft control interface;
若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令;及If the touch operation is detected, acquiring sensor data, and obtaining an aircraft manipulation command based on at least the sensor data; and
向飞行器发送所述飞行器操控指令。The aircraft maneuver command is sent to the aircraft.
一种移动终端,包括存储器和处理器,所述存储器中储存有计算机可读指令,所述计算机可读指令被所述处理器执行时,使得所述处理器执行以下步骤:A mobile terminal comprising a memory and a processor, the memory storing computer readable instructions, the computer readable instructions being executed by the processor, such that the processor performs the following steps:
显示飞行器操控界面;Display the aircraft control interface;
检测作用于所述飞行器操控界面的触控操作;Detecting a touch operation acting on the aircraft control interface;
若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令;及If the touch operation is detected, acquiring sensor data, and obtaining an aircraft manipulation command based on at least the sensor data; and
向飞行器发送所述飞行器操控指令。The aircraft maneuver command is sent to the aircraft.
一个或多个存储有计算机可读指令的计算机可读非易失性存储介质,所述计算机可读指令被一个或多个处理器执行时,使得所述一个或多个处理器执行以下步骤:One or more computer readable non-volatile storage media storing computer readable instructions, when executed by one or more processors, cause the one or more processors to perform the steps of:
显示飞行器操控界面;Display the aircraft control interface;
检测作用于所述飞行器操控界面的触控操作;Detecting a touch operation acting on the aircraft control interface;
若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令;及If the touch operation is detected, acquiring sensor data, and obtaining an aircraft manipulation command based on at least the sensor data; and
向飞行器发送所述飞行器操控指令。The aircraft maneuver command is sent to the aircraft.
本发明的一个或多个实施例的细节在下面的附图和描述中提出。本发明的其它特征、目的和优点将从说明书、附图以及权利要求书变得明显。Details of one or more embodiments of the invention are set forth in the accompanying drawings and description below. Other features, objects, and advantages of the invention will be apparent from the description and appended claims.
附图说明DRAWINGS
为了更清楚地说明本发明实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作简单地介绍,显而易见地,下面 描述中的附图仅仅是本发明的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the description of the prior art will be briefly described below, obviously, the following The drawings in the description are only some of the embodiments of the present invention, and those skilled in the art can obtain other drawings based on these drawings without any creative work.
图1为一个实施例中飞行器操控系统的应用环境图;1 is an application environment diagram of an aircraft handling system in an embodiment;
图2为一个实施例中应用飞行器操控方法的移动终端的结构示意图;2 is a schematic structural diagram of a mobile terminal applying an aircraft handling method in an embodiment;
图3为一个实施例中飞行器的结构示意图;Figure 3 is a schematic structural view of an aircraft in an embodiment;
图4为一个实施例中飞行器操控方法的流程示意图;4 is a schematic flow chart of an aircraft handling method in an embodiment;
图5为一个实施例中移动终端显示的展示页面的示意图;FIG. 5 is a schematic diagram of a display page displayed by a mobile terminal in an embodiment; FIG.
图6为一个实施例中移动终端显示的飞行器操控界面的示意图;6 is a schematic diagram of an aircraft control interface displayed by a mobile terminal in an embodiment;
图7为一个实施例中根据对第二触控区域的触摸操作操控飞行器的步骤的流程示意图;7 is a schematic flow chart of a step of manipulating an aircraft according to a touch operation on a second touch area in one embodiment;
图8为一个实施例中飞行器操控界面的示意图;Figure 8 is a schematic illustration of an aircraft handling interface in one embodiment;
图9为一个实施例中传感器数据得到飞行器操控指令的步骤的流程示意图;9 is a flow chart showing the steps of obtaining sensor control commands from sensor data in an embodiment;
图10为一个实施例中用户按住第一触控区域朝四个主方向挥动移动终端以操控飞行器分别执行四种动作的手势示意图;10 is a schematic diagram of a gesture in which the user swipes the mobile terminal in four main directions by pressing the first touch area to control the aircraft to perform four actions respectively;
图11为一个实施例中移动终端对用户按住第一触控区域朝第一个方向挥动移动终端进行动作示例的示意图;11 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a first direction in an embodiment;
图12为一个实施例中移动终端对用户按住第一触控区域朝第二个方向挥动移动终端进行动作示例的示意图;12 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a second direction in an embodiment;
图13为一个实施例中移动终端对用户按住第一触控区域朝第三个方向挥动移动终端进行动作示例的示意图;FIG. 13 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a third direction in an embodiment; FIG.
图14为一个实施例中移动终端对用户按住第一触控区域朝第四个方向挥动移动终端进行动作示例的示意图;14 is a schematic diagram showing an example of an action performed by a mobile terminal to a user to hold a first touch area and swing a mobile terminal in a fourth direction in an embodiment;
图15为一个实施例中选择预设自动操控模式操控飞行器的步骤的流程示意图;15 is a flow chart showing the steps of selecting a preset automatic control mode to operate an aircraft in one embodiment;
图16为一个实施例中移动终端的结构框图;16 is a structural block diagram of a mobile terminal in an embodiment;
图17为另一个实施例中移动终端的结构框图; 17 is a structural block diagram of a mobile terminal in another embodiment;
图18为一个实施例中传感器数据处理模块的结构框图;18 is a structural block diagram of a sensor data processing module in an embodiment;
图19为再一个实施例中移动终端的结构框图。Figure 19 is a block diagram showing the structure of a mobile terminal in still another embodiment.
具体实施方式detailed description
为了使本发明的目的、技术方案及优点更加清楚明白,以下结合附图及实施例,对本发明进行进一步详细说明。应当理解,此处所描述的具体实施例仅仅用以解释本发明,并不用于限定本发明。The present invention will be further described in detail below with reference to the accompanying drawings and embodiments. It is understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.
如图1所示,在一个实施例中,提供了一种飞行器操控系统100,包括移动终端102和飞行器104。移动终端102和飞行器104之间建立无线连接,通过该无线连接来在移动终端102和飞行器104之间传输数据。飞行器104是可被遥控的飞行装置,可以是无人机,具体可以是固定翼无人机、旋翼无人机、伞翼无人机、扑翼无人机和无人飞艇中的任意一种,飞行器104还可以是带动力的航空模型。As shown in FIG. 1, in one embodiment, an aircraft handling system 100 is provided that includes a mobile terminal 102 and an aircraft 104. A wireless connection is established between the mobile terminal 102 and the aircraft 104 by which data is transferred between the mobile terminal 102 and the aircraft 104. The aircraft 104 is a flight device that can be remotely controlled, and may be a drone, and specifically may be any one of a fixed-wing drone, a rotor-wing drone, a wing-wing drone, a flapping drone, and an unmanned airship. The aircraft 104 can also be a powered aviation model.
如图2所示,在一个实施例中,提供了一种移动终端102,包括通过系统总线连接的处理器、非易失性存储介质、内存储器、通信装置、显示屏和输入装置。其中处理器具有计算功能和控制移动终端102工作的功能,该处理器被配置为执行一种飞行器操控方法。非易失性存储介质包括磁存储介质、光存储介质以及闪存式存储介质中的至少一种。非易失性存储介质存储有操作系统。非易失性存储介质或内存储器可存储有计算机可读指令,该计算机可读指令被处理器执行时,可使得处理器执行一种飞行器操控方法。内存储器用于为操作系统和计算机可读指令提供高速缓存。通信装置用于与飞行器104进行无线通信。显示屏包括液晶显示屏、柔性显示屏和电子墨水显示屏中的至少一种。输入装置包括物理按钮、轨迹球、触控板以及与显示屏重叠的触控层中的至少一种,其中触控层与显示屏组合形成触控屏。移动终端102可以是手机、平板电脑、PDA(个人数字助理)以及触控遥控器中的至少一种。As shown in FIG. 2, in one embodiment, a mobile terminal 102 is provided that includes a processor coupled via a system bus, a non-volatile storage medium, an internal memory, a communication device, a display screen, and an input device. Wherein the processor has computing functionality and functionality to control operation of the mobile terminal 102, the processor being configured to perform an aircraft handling method. The non-volatile storage medium includes at least one of a magnetic storage medium, an optical storage medium, and a flash storage medium. The non-volatile storage medium stores an operating system. The non-volatile storage medium or internal memory can store computer readable instructions that, when executed by the processor, cause the processor to perform an aircraft manipulation method. The internal memory is used to provide a cache for the operating system and computer readable instructions. The communication device is for wireless communication with the aircraft 104. The display includes at least one of a liquid crystal display, a flexible display, and an electronic ink display. The input device includes at least one of a physical button, a trackball, a touchpad, and a touch layer overlapping the display screen, wherein the touch layer and the display screen are combined to form a touch screen. The mobile terminal 102 may be at least one of a mobile phone, a tablet, a PDA (Personal Digital Assistant), and a touch remote control.
如图3所示,在一个实施例中,提供了一种飞行器104,包括通过系统 总线连接的处理器、非易失性存储介质、内存储器、通信装置、飞行驱动装置、拍摄装置和定位装置。其中处理器具有计算功能和控制飞行器104工作的功能,该处理器被配置为执行来自于移动终端的操控指令或者组合操控指令。非易失性存储介质包括磁存储介质、光存储介质以及闪存式存储介质中的至少一种。非易失性存储介质存储有操作系统和用于执行来自于移动终端的操控指令或者组合操控指令的操控指令执行装置。内存储器用于为操作系统和操控指令执行装置提供高速缓存。通信装置用于与移动终端102进行无线通信。飞行驱动装置用于控制飞行器104的飞行器飞行动作,主要通过控制飞行器104的飞行速度和飞行方向来控制飞行器飞行动作。对于旋翼飞行器,飞行驱动装置主要包括旋翼及旋翼控制装置。拍摄装置用于拍摄图像,拍摄的图像包括图片和视频。定位装置可以是GPS(Global Positioning System,全球定位系统)定位装置,用于定位飞行器104的位置。As shown in FIG. 3, in one embodiment, an aircraft 104 is provided, including a pass system Bus-connected processor, non-volatile storage medium, internal memory, communication device, flight drive, camera, and positioning device. Wherein the processor has a computing function and a function to control the operation of the aircraft 104, the processor being configured to execute a manipulation command or a combination manipulation command from the mobile terminal. The non-volatile storage medium includes at least one of a magnetic storage medium, an optical storage medium, and a flash storage medium. The non-volatile storage medium stores an operating system and a manipulation instruction execution device for executing a manipulation command or a combination manipulation command from the mobile terminal. The internal memory is used to provide a cache for the operating system and the manipulation instruction execution device. The communication device is for wirelessly communicating with the mobile terminal 102. The flight drive is used to control the flight behavior of the aircraft of the aircraft 104, primarily by controlling the flight speed and flight direction of the aircraft 104. For rotorcraft, the flight drive mainly includes rotor and rotor control devices. The camera is used to capture images, including images and videos. The positioning device may be a GPS (Global Positioning System) positioning device for locating the position of the aircraft 104.
如图4所示,在一个实施例中,提供了一种飞行器操控方法,本实施例以该方法应用于上述图1和图2中的移动终端102来举例说明。该方法包括如下步骤:As shown in FIG. 4, in one embodiment, an aircraft maneuvering method is provided. This embodiment is exemplified by the method applied to the mobile terminal 102 of FIGS. 1 and 2 described above. The method comprises the following steps:
步骤402,显示飞行器操控界面。 Step 402, displaying an aircraft manipulation interface.
具体地,移动终端上运行有飞行器操控应用,该飞行器操控应用具有操控飞行器的功能,还可以具有对飞行器拍摄的照片或者视频进行处理的功能,这里对飞行器拍摄的照片或者视频进行处理主要包括分类、展示、向社交好友分享以及生成行进路线。移动终端具体可按照照片或者视频的拍摄时间进行排序生成行进路线,还可以将拍摄照片或者视频时记录的地理位置信息按照相应的拍摄时间进行排序生成行进路线。这里的行进路线可以体现飞行器的行进路线,也可以进一步体现用户的行进路线。Specifically, the mobile terminal runs an aircraft control application, and the aircraft control application has the function of manipulating the aircraft, and may also have a function of processing photos or videos taken by the aircraft, where the processing of the photos or videos taken by the aircraft mainly includes classification. , show, share with social friends, and generate travel routes. The mobile terminal may specifically sort the travel route according to the shooting time of the photo or video, and may also sort the geographic location information recorded when the photo or video is taken according to the corresponding shooting time to generate a travel route. The travel route here can reflect the travel route of the aircraft, and can further reflect the travel route of the user.
移动终端通过飞行器操控应用提供用于触发飞行器操控指令的飞行器操控界面,具体可在用于展示飞行器拍摄的照片或者视频的展示页面跳转到飞行器操控界面。举例说明,移动终端运行飞行器操控应用,首先进入如图5所示的展示页面,用户在该展示页面中可以分类查看飞行器拍摄的照片或者 视频并向社交好友分享,还可以展示根据飞行器拍摄的照片或者视频生成的进行路线。移动终端在检测到对飞行器操控图标502的操作时进入如图6所示的飞行器操控界面。The mobile terminal provides an aircraft control interface for triggering aircraft maneuver commands through the aircraft control application, specifically to the aircraft control interface on a display page for displaying photos or videos taken by the aircraft. For example, the mobile terminal runs the aircraft control application, first enters the display page as shown in FIG. 5, and the user can classify and view the photos taken by the aircraft in the display page or The video is shared with social friends, and it can also show the route generated based on the photos or videos taken by the aircraft. The mobile terminal enters the aircraft control interface as shown in FIG. 6 upon detecting the operation of the aircraft control icon 502.
步骤404,检测作用于飞行器操控界面的触控操作。 Step 404, detecting a touch operation acting on the aircraft control interface.
具体地,第一触控区域是飞行器操控界面中的特定区域,用于承受触控操作的作用。第一触控区域可以是按钮,该按钮默认为第一状态,在检测到触控操作时变化为第二状态,这里的状态包括形状、颜色和图案中的至少一种,比如按钮默认为凸起状态,在检测到触控操作之后变化为下沉状态。第一触控区域也可以是用预设标记标识出的区域,比如用虚框圈起来或者用特殊颜色标识出的区域。第一触控区域也可以不进行标识,而是通过在首次进入飞行器操控界面时的引导图示进行指示。触控操作具体可以是触摸点击操作、触摸双击操作、触摸长按操作、滑动操作以及多点触控操作,多点触控操作是基于多个触控点的操作,比如触发多个触控点后将多个触控点汇集,或者触发多个触控点后将多个触控点扩散等。触控操作作用于第一触控区域,是指触控操作的触控点在第一触控区域内。移动终端可实时或者定期检测作用于飞行器操控界面的触控操作。Specifically, the first touch area is a specific area in the aircraft control interface for supporting the touch operation. The first touch area may be a button, and the button defaults to the first state, and changes to the second state when the touch operation is detected, where the state includes at least one of a shape, a color, and a pattern, for example, the button is convex by default. The up state changes to a sinking state after the touch operation is detected. The first touch area may also be an area identified by a preset mark, such as an area circled by a virtual frame or identified by a special color. The first touch area may also be unmarked, but instead indicated by a guide icon when entering the aircraft control interface for the first time. The touch operation may specifically be a touch click operation, a touch double click operation, a touch long press operation, a sliding operation, and a multi-touch operation, and the multi-touch operation is based on operations of multiple touch points, such as triggering multiple touch points. After that, multiple touch points are collected, or multiple touch points are triggered, and then multiple touch points are spread. The touch operation is applied to the first touch area, and the touch point of the touch operation is in the first touch area. The mobile terminal can detect the touch operation acting on the aircraft control interface in real time or periodically.
举例说明,参照图6,第一触控区域可以是位于飞行器操控界面中的区域602,用户通过触摸体触摸第一触控区域602并保持触控点不消失,则移动终端会检测到作用于该第一触控区域602的触控操作。触摸体比如触控笔或者用户的手指。For example, referring to FIG. 6 , the first touch area may be an area 602 located in the aircraft control interface. When the user touches the first touch area 602 through the touch body and keeps the touch point from disappearing, the mobile terminal may detect the action. The touch operation of the first touch area 602. A touch body such as a stylus or a user's finger.
步骤406,若检测到触控操作,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令。Step 406: If the touch operation is detected, the sensor data is acquired, and the aircraft manipulation command is obtained according to at least the sensor data.
移动终端具体可通过读取传感器数据的接口从相应的传感器读取传感器数据,其中传感器数据可以是多个传感器的传感器数据。在一个实施例中,传感器数据来自于方向传感器、重力传感器、加速度传感器、光线传感器、电子罗盘、距离传感器、三轴陀螺仪传感器、温度传感器以及压力传感器中的至少一种。 The mobile terminal can specifically read the sensor data from the corresponding sensor through an interface that reads the sensor data, wherein the sensor data can be sensor data of the plurality of sensors. In one embodiment, the sensor data is from at least one of a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor.
移动终端可根据传感器数据和飞行器操控指令的映射关系,以及获取到的传感器数据,得到飞行器操控指令。传感器数据和飞行器操控指令的映射关系可用函数来表示,该函数的自变量可以是传感器数据,因变量可以是所映射的飞行器操控指令的标识。The mobile terminal can obtain an aircraft manipulation command according to the mapping relationship between the sensor data and the aircraft manipulation command, and the acquired sensor data. The mapping relationship between the sensor data and the aircraft maneuver command can be represented by a function, the argument of the function can be sensor data, and the dependent variable can be the identifier of the mapped aircraft maneuver instruction.
其中飞行器操控指令可以是控制飞行器飞行状态以及飞行器姿态的操控指令,也可以是控制飞行器拍摄照片或者视频的操控指令,还可以是其它用来操控飞行器执行某动作的指令。其中飞行状态比如飞行方向、飞行速度、飞行高度、悬停以及飞行目的地等中的至少一种,飞行器姿态比如侧身或者旋转等。The aircraft control command may be a control command for controlling the flight state of the aircraft and the attitude of the aircraft, or may be a control command for controlling the aircraft to take a photo or video, or may be other instructions for controlling the aircraft to perform an action. The flight state such as at least one of a flight direction, a flight speed, a flying height, a hover, and a flight destination, the attitude of the aircraft such as a side body or a rotation.
举例说明,若传感器数据为来自于压力传感器的压力数值,或者为来自于温度传感器的温度数值,或者为来自于光线传感器的光亮度值,则可根据传感器数据得到用于控制飞行器飞行速度的飞行器操控指令,比如压力数值越大飞行器飞行越快,或者温度数值越大飞行器飞行越快。若传感器数据为来自于距离传感器的距离值,则可根据传感器数据得到用于在距离值小于第一预设值时减速且在小于第二预设值时停止前进的飞行器操控指令,其中第一预设值大于第二预设值。For example, if the sensor data is a pressure value from a pressure sensor, or a temperature value from a temperature sensor, or a lightness value from a light sensor, an aircraft for controlling the flight speed of the aircraft can be obtained based on the sensor data. Manipulating commands, such as the higher the pressure value, the faster the aircraft flies, or the higher the temperature, the faster the aircraft flies. If the sensor data is a distance value from the distance sensor, an aircraft control command for decelerating when the distance value is less than the first preset value and stopping when the distance value is less than the second preset value may be obtained according to the sensor data, where the first The preset value is greater than the second preset value.
步骤408,向飞行器发送飞行器操控指令。 Step 408, transmitting an aircraft manipulation command to the aircraft.
具体地,移动终端将根据传感器数据获得的飞行器操控指令通过与飞行器的无线连接发送给飞行器,使得飞行器接收到飞行器操控指令后执行飞行器操控指令所指定的动作。飞行器若接收到多个飞行器操控指令,则可按照接收顺序依次执行各飞行器操控指令所指定的动作。Specifically, the mobile terminal transmits the aircraft manipulation command obtained according to the sensor data to the aircraft through a wireless connection with the aircraft, so that the aircraft performs the action specified by the aircraft manipulation command after receiving the aircraft manipulation command. If the aircraft receives a plurality of aircraft maneuver commands, the actions specified by the respective aircraft maneuver commands may be sequentially executed in the order of reception.
上述飞行器操控方法,显示飞行器操控界面,该飞行器操控界面具有第一触控区域,若检测到作用于第一触控区域的触控操作时,利用传感器数据来生成飞行器操控指令发送给飞行器。这样用户在通过触控操作作用于第一触控区域时,便可以通过改变传感器所检测到的传感器数据来实现对飞行器的操控,提供了一种简单而且全新的操控方式,使得用户在操控飞行器时有更多的选择,对飞行器的操控更加方便。 The aircraft control method displays an aircraft control interface, and the aircraft control interface has a first touch area. When the touch operation on the first touch area is detected, the sensor data is used to generate an aircraft control command and sent to the aircraft. In this way, when the user acts on the first touch area through the touch operation, the user can control the aircraft by changing the sensor data detected by the sensor, and provides a simple and brand-new control mode, so that the user is manipulating the aircraft. There are more choices and it is more convenient to control the aircraft.
在一个实施例中,步骤406包括:若检测到作用于飞行器操控界面中第一触控区域的用于开启传感器控制模式的第一触控操作,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至检测到作用于第一触控区域的第二触控操作时停止。In one embodiment, step 406 includes: if the first touch operation for opening the sensor control mode in the first touch area of the aircraft control interface is detected, acquiring sensor data, and obtaining the aircraft based on at least the sensor data. The command is commanded until the second touch operation acting on the first touch area is detected to stop.
具体地,移动终端检测的触控操作包括用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作。传感器控制模式是指通过传感器数据来操控飞行器的模式,移动终端在开启传感器控制模式后获取传感器数据并至少根据传感器数据得到飞行器操控指令,并将飞行器操控指令发送到飞行器。移动终端在关闭传感器控制模式后将不再获取传感器数据,或者不再至少根据传感器数据得到飞行器操控指令,或者不再将飞行器操控指令发送到飞行器,而是可以通过其它方式操控飞行器,比如通过模拟摇杆操控飞行器。Specifically, the touch operation detected by the mobile terminal includes a first touch operation for turning on the sensor control mode and a second touch operation for turning off the sensor control mode. The sensor control mode refers to a mode in which the aircraft is manipulated by sensor data. The mobile terminal acquires sensor data after turning on the sensor control mode and obtains an aircraft control command based on at least the sensor data, and transmits the aircraft control command to the aircraft. After the mobile terminal turns off the sensor control mode, the sensor data will no longer be acquired, or the aircraft control command will no longer be obtained according to the sensor data, or the aircraft control command will not be sent to the aircraft, but the aircraft can be manipulated by other means, such as by simulation. The joystick controls the aircraft.
本实施例中,通过分别用于开启和关闭传感器控制模式的触控操作,可以灵活地控制进入传感器控制模式的时机,从而在传感器控制模式下利用传感器所检测到的传感器数据的变化来操控飞行器,对飞行器的操控更加便捷。In this embodiment, the timing of entering the sensor control mode can be flexibly controlled by the touch operation for turning the sensor control mode on and off, respectively, thereby using the change of the sensor data detected by the sensor to control the aircraft in the sensor control mode. The handling of the aircraft is more convenient.
在一个实施例中,用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作可以相同。此时触控操作可从触摸点击操作、触摸双击操作、滑动操作以及多点触控操作中选择。In one embodiment, the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be the same. At this time, the touch operation can be selected from a touch click operation, a touch double click operation, a slide operation, and a multi-touch operation.
比如若检测到对第一触控区域的一次触摸点击操作,则开启传感器控制模式,进而获取传感器数据,并至少根据传感器数据得到飞行器操控指令,向飞行器发送飞行器操控指令。若再次检测到对第一触控区域的一次触摸点击操作,则关闭传感器控制模式。For example, if a touch click operation on the first touch area is detected, the sensor control mode is turned on, and the sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the aircraft control command is sent to the aircraft. If a touch click operation on the first touch area is detected again, the sensor control mode is turned off.
在一个实施例中,用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作可以不相同。此时两种触控操作可分别从触摸点击操作、触摸双击操作、滑动操作以及多点触控操作中选择。In one embodiment, the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be different. At this time, the two touch operations can be selected from a touch click operation, a touch double click operation, a slide operation, and a multi-touch operation, respectively.
比如若检测到对第一触控区域的触摸点击操作,则开启传感器控制模式,进而获取传感器数据,并至少根据传感器数据得到飞行器操控指令,向飞行 器发送飞行器操控指令。若检测到对第一触控区域的触摸双击操作,则关闭传感器控制模式。For example, if a touch click operation on the first touch area is detected, the sensor control mode is turned on, and sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the flight is performed. The aircraft sends an aircraft control command. If a touch double click operation on the first touch area is detected, the sensor control mode is turned off.
在一个实施例中,用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作可以包含于一个组合触控操作中。组合触控操作比如触摸长按操作,包括触发触摸长按操作的触控操作和解除触摸长按操作的触控操作。In one embodiment, the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be included in one combined touch operation. The combined touch operation, such as a touch long press operation, includes a touch operation that triggers a long press operation and a touch operation that releases a long press operation.
在一个实施例中,步骤406包括:自检测到第三触控操作起开始计时,若计时达到预设时长且第三触控操作保持作用于飞行器操控界面中的第一触控区域,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至第三触控操作停止。In one embodiment, the step 406 includes: starting from the detection of the third touch operation, and if the timing reaches the preset duration and the third touch operation remains applied to the first touch area in the aircraft control interface, acquiring The sensor data, and at least the aircraft control command is obtained according to the sensor data until the third touch operation is stopped.
具体地,本实施例中检测的第三触控操作为持续触控操作,移动终端在检测到该第三触控操作后,在该第三触控操作对第一触控区域的所用时间内,获取传感器数据,并至少根据传感器数据得到飞行器操控指令,以及向飞行器发送飞行器操控指令,直至触控点对第一触控区域的作用消失。其中触控操作的作用时间是指从检测到该触控操作的时刻到该触控操作消失的时间段。Specifically, the third touch operation detected in the embodiment is a continuous touch operation, and the mobile terminal detects the third touch operation after the third touch operation is used for the first touch area. Obtaining sensor data, and at least obtaining an aircraft control command according to the sensor data, and transmitting an aircraft control command to the aircraft until the effect of the touch point on the first touch area disappears. The action time of the touch operation refers to a time period from when the touch operation is detected to when the touch operation disappears.
其中,预设时长是为了与点触操作区分,若检测到触控点起的预设时长之内该触控点消失,则识别为点触操作,若达到预设时长触控点仍未消失,则识别为需要检测的持续的触控操作,进入传感器控制模式。自检测到第三触控操作的触控点起开始计时并计时达到预设时长,是用于开启传感器控制模式的第一触控操作,触控点对第一触控区域的作用消失则是用于关闭传感器控制模式的第二触控操作。The preset duration is for distinguishing from the touch operation. If the touch point disappears within the preset duration from the detection of the touch point, the touch operation is recognized as a touch operation, and the touch point does not disappear if the preset time is reached. , it is recognized as a continuous touch operation that needs to be detected, and enters the sensor control mode. The first touch operation for turning on the sensor control mode is started when the touch point of the third touch operation is detected and the time is up to the preset time. The effect of the touch point on the first touch area disappears. A second touch operation for turning off the sensor control mode.
本实施例中,在检测到触控点起开始计时,若达到预设时长触控点仍保持作用于第一触控区域,可防止因用户误触第一触控区域而造成飞行器失控。In this embodiment, when the touch point is detected, the time is started. If the touch time is still applied to the first touch area when the preset time is reached, the aircraft may be prevented from being out of control due to the user accidentally touching the first touch area.
在其它实施例中,移动终端也可在检测到触控操作之后立即获取传感器数据,并至少根据传感器数据得到飞行器操控指令,以及向飞行器发送飞行器操控指令,直至触控点对第一触控区域的作用消失。 In other embodiments, the mobile terminal may also acquire sensor data immediately after detecting the touch operation, and at least obtain an aircraft control command according to the sensor data, and send an aircraft control command to the aircraft until the touch point is opposite to the first touch area. The role disappears.
如图7所示,在一个实施例中,该方法还包括根据对第二触控区域的触摸操作操控飞行器的步骤,具体包括如下步骤:As shown in FIG. 7 , in an embodiment, the method further includes the step of manipulating the aircraft according to the touch operation on the second touch area, and specifically includes the following steps:
步骤702,检测作用于飞行器操控界面中第二触控区域的触摸操作;第二触控区域用于模拟摇杆操作。Step 702: detecting a touch operation applied to the second touch area in the aircraft control interface; the second touch area is used to simulate the joystick operation.
具体地,第二触控区域是飞行器操控界面中的特定区域,用于承受触摸操作来模拟摇杆操作。触摸操作比如触摸点击操作、触摸双击操作、触摸长按操作、滑动操作以及多点触控操作。作用于第二触控区域的触摸操作与作用于第一触控区域的触控操作分别实现不同的操控方式。Specifically, the second touch area is a specific area in the aircraft manipulation interface for withstanding a touch operation to simulate a joystick operation. Touch operations such as touch click operations, touch double tap operations, touch long press operations, swipe operations, and multi-touch operations. The touch operation applied to the second touch area and the touch operation applied to the first touch area respectively implement different control modes.
在一个实施例中,第二触控区域可以包围第一触控区域,此时第二触控区域与第一触控区域不重叠,触摸操作与检测的触控操作可以存在相同的情况。在其它实施例中,第二触控区域可与第一触控区域相分离。In one embodiment, the second touch area can surround the first touch area. The second touch area does not overlap with the first touch area. The touch operation and the detected touch operation may be the same. In other embodiments, the second touch area can be separated from the first touch area.
步骤704,获取触摸操作所触发的模拟摇杆操控指令。Step 704: Acquire an analog joystick manipulation command triggered by the touch operation.
步骤706,向飞行器发送模拟摇杆操控指令。In step 706, an analog joystick manipulation command is sent to the aircraft.
具体地,触摸操作作用于第二触控区域的不同区域,可分别触发不同的模拟摇杆操控指令。具体第二触控区域中可定义四个主方向,比如上下左右,从而移动终端可根据触摸操作作用于第二触控区域中相对于四个主方向的相对位置来触发相应的模拟摇杆操控指令。模拟摇杆操控指令与飞行器操控指令不冲突。优选地,模拟摇杆操控指令用于操控飞行器垂直升降和飞行器姿态的变化,飞行器操控指令用于操控飞行器沿水平面的各方向的移动。Specifically, the touch operation acts on different regions of the second touch area, and different analog joystick manipulation commands can be triggered respectively. The specific second touch area can define four main directions, such as up, down, left and right, so that the mobile terminal can trigger the corresponding analog joystick control according to the relative position of the second touch area relative to the four main directions according to the touch operation. instruction. The analog joystick control command does not conflict with the aircraft control command. Preferably, the analog rocker steering command is used to manipulate the vertical movement of the aircraft and the change in attitude of the aircraft, and the aircraft maneuver command is used to manipulate the movement of the aircraft in various directions along the horizontal plane.
参照图8,若触摸操作的触控点作用于第二触控区域801的主方向上,如图8中四个手势802、803、804以及805所表示的触摸操作,则移动终端可触发该主方向所对应的模拟摇杆操控指令,将模拟摇杆操控指令发送到飞行器之后,飞行器可根据接收到的模拟摇杆操控指令实施上升、下降、左旋或者右旋的动作。Referring to FIG. 8 , if the touch point of the touch operation acts on the main direction of the second touch area 801, as shown by the four gestures 802, 803, 804, and 805 in FIG. 8 , the mobile terminal may trigger the touch operation. After the analog joystick manipulation command corresponding to the main direction is sent to the aircraft, the aircraft can perform the ascending, descending, left-handed or right-handed motion according to the received analog joystick manipulation command.
若触摸操作作用于第二触控区域中主方向之外的位置,则移动终端可根据触摸操作的触控点映射在主方向上的分量来触发相应的组合的模拟摇杆操控指令,将组合的模拟摇杆操控指令发送到飞行器,飞行器可根据接收到的 组合的模拟摇杆操控指令实施左旋上升、右旋上升、左旋下降或者右旋下降的动作。If the touch operation is applied to a position other than the main direction in the second touch area, the mobile terminal may trigger the corresponding combined analog joystick manipulation command according to the component of the touch operation mapped by the touch point in the main direction, and combine The analog joystick manipulation command is sent to the aircraft, and the aircraft can be received according to the The combined analog joystick manipulation command performs a left-handed rise, a right-handed rise, a left-handed fall, or a right-handed down action.
本实施例中,移动终端检测作用于飞行器操控界面的触控操作,并检测作用于飞行器操控界面的第二触控区域的触摸操作,从而根据不同的检测结果的组合来实现飞行器的不同的操控方式。这样使得飞行器的操控方式更加多样化,对飞行器的操控更加灵活、方便。In this embodiment, the mobile terminal detects a touch operation applied to the aircraft control interface, and detects a touch operation of the second touch area acting on the aircraft control interface, thereby implementing different operations of the aircraft according to a combination of different detection results. the way. This makes the aircraft's control mode more diverse, and the handling of the aircraft is more flexible and convenient.
在一个实施例中,步骤406包括:若检测到第四触控操作的触控点作用于第一触控区域,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至触控点消失时停止。该方法还包括:当触控点移动到飞行器操控界面中的第二触控区域时,根据触控点在第二触控区域中的位置触发模拟摇杆操控指令并发送到飞行器;第二触控区域用于模拟摇杆操作。In one embodiment, step 406 includes: if it is detected that the touch point of the fourth touch operation acts on the first touch area, acquiring sensor data, and at least obtaining an aircraft control command according to the sensor data until the touch point disappears Stop when. The method further includes: when the touch point moves to the second touch area in the aircraft control interface, triggering the analog joystick manipulation command according to the position of the touch point in the second touch area and transmitting to the aircraft; the second touch The control area is used to simulate the joystick operation.
具体地,本实施例中检测的第四触控操作为持续触控操作,移动终端在检测到该第四触控操作后,在相应的触控点的作用时间内,获取传感器数据,并至少根据传感器数据得到飞行器操控指令,以及向飞行器发送飞行器操控指令,直至触控点消失。其中,检测到第四触控操作的触控点作用于第一触控区域,是用于开启传感器控制模式的第一触控操作,触控点消失则是用于关闭传感器控制模式的第二触控操作。Specifically, the fourth touch operation detected in the embodiment is a continuous touch operation, and after detecting the fourth touch operation, the mobile terminal acquires sensor data during the action time of the corresponding touch point, and at least The aircraft control command is obtained based on the sensor data, and the aircraft control command is sent to the aircraft until the touch point disappears. The touch point that detects the fourth touch operation acts on the first touch area, and is the first touch operation for turning on the sensor control mode, and the touch point disappears is the second method for turning off the sensor control mode. Touch operation.
移动终端也可以自检测到第四触控操作的触控点起开始计时,若计时达到预设时长且相应的触控点保持作用于第一触控区域,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至该触控点消失时停止。其中,自检测到第四触控操作的触控点起开始计时并计时达到预设时长,是用于开启传感器控制模式的第一触控操作,触控点消失则是用于关闭传感器控制模式的第二触控操作。The mobile terminal can also start timing when the touch point of the fourth touch operation is detected. If the time reaches the preset time and the corresponding touch point remains in the first touch area, the sensor data is acquired, and at least according to the sensor. The data is obtained by the aircraft control command until the touch point disappears. The first touch operation for turning on the sensor control mode is started when the touch point of the fourth touch operation is detected and the timing is reached, and the touch point disappears to close the sensor control mode. The second touch operation.
进一步地,当触控点移动到飞行器操控界面中的第二触控区域时,便可以触发上述步骤702至706,此时触控点对第二触控区域的作用为作用于第二触控区域的触摸操作。Further, when the touch point moves to the second touch area in the aircraft control interface, the steps 702 to 706 can be triggered, and the action of the touch point on the second touch area acts on the second touch. The touch operation of the area.
本实施例中,通过连续的第四触控操作,可以相继触发进入传感器控制 模式以及模拟摇杆操控飞行器,可实现单手操控飞行器,使得飞行器的操控更加方便、快捷。In this embodiment, the continuous sensor touch control can be sequentially triggered by the fourth touch operation. The mode and the analog joystick control aircraft can realize the one-handed operation of the aircraft, making the operation of the aircraft more convenient and faster.
在一个实施例中,步骤406包括:检测作用于飞行器操控界面中第二触控区域一触控按钮的按压触摸操作,检测到时,获取传感器数据;检测触控按钮跟随按压触摸操作在第二触控区域或飞行器操控界面中的移动,根据移动获取模拟摇杆操控指令;根据传感器数据以及模拟摇杆操控指令得到飞行器操控指令。In one embodiment, step 406 includes: detecting a touch touch operation of a touch button applied to the second touch area of the aircraft control interface, and detecting sensor data when detecting; detecting the touch button following the touch operation at the second The movement in the touch area or the aircraft control interface acquires an analog joystick manipulation command according to the movement; the aircraft manipulation command is obtained according to the sensor data and the analog joystick manipulation command.
其中,模拟摇杆操控指令是模拟摇杆遥控器的操控指令,具体可在第二触控区域中定义四个主方向,比如上下左右,从而可根据按压触摸操作作用于第二触控区域中相对于四个主方向的相对位置来触发相应的模拟摇杆操控指令。模拟摇杆操控指令与飞行器操控指令不冲突。优选地,模拟摇杆操控指令用于操控飞行器垂直升降和飞行器姿态的变化。The analog joystick control command is a control command of the analog joystick remote control, and specifically defines four main directions in the second touch area, such as up, down, left, and right, so that the touch operation can be applied to the second touch area according to the pressing touch operation. The corresponding analog joystick manipulation command is triggered relative to the relative positions of the four main directions. The analog joystick control command does not conflict with the aircraft control command. Preferably, the analog rocker steering command is used to manipulate the vertical movement of the aircraft and the change in attitude of the aircraft.
本实施例中,通过第二触控区域一触控按钮的按压触摸操作,可以相继触发进入传感器控制模式以及模拟摇杆操控飞行器,可实现单手操控飞行器,使得飞行器的操控更加方便、快捷。In this embodiment, by pressing and touching the touch control button of the second touch area, the sensor control mode and the analog joystick control aircraft can be successively triggered, and the aircraft can be operated by one hand, so that the operation of the aircraft is more convenient and faster.
如图9所示,在一个实施例中,至少根据传感器数据得到飞行器操控指令的步骤具体包括以下步骤:As shown in FIG. 9, in one embodiment, the step of obtaining an aircraft manipulation command based on at least the sensor data specifically includes the following steps:
步骤902,根据获取的初始的传感器数据确定传感器所在移动终端的初始状态。Step 902: Determine an initial state of the mobile terminal where the sensor is located according to the obtained initial sensor data.
具体地,传感器数据包括用于反映移动终端的姿态和运动中的至少一种的数据。初始的传感器数据是移动终端在进入传感器控制模式之后最初收到的传感器数据,用来确定移动终端当前所处的状态,定义为初始状态。初始状态包括移动终端的姿态状态和运动状态,其中姿态状态包括移动终端倾斜的部分、倾斜的方向以及倾斜角度等,运动状态包括运动速度、运动加速度以及运动方向等。Specifically, the sensor data includes data for reflecting at least one of a posture and a motion of the mobile terminal. The initial sensor data is the sensor data initially received by the mobile terminal after entering the sensor control mode, and is used to determine the current state of the mobile terminal, which is defined as an initial state. The initial state includes an attitude state and a motion state of the mobile terminal, wherein the posture state includes a tilted portion of the mobile terminal, a tilted direction, and a tilt angle, and the like, and the motion state includes a motion speed, a motion acceleration, and a motion direction.
移动终端可根据移动终端的三维固定参考坐标系确定移动终端在三维空间中的初始状态。其中,若固定参考坐标系为三维参考坐标系,包括相互垂 直的三轴,其中两轴可以平行于移动终端的显示屏,而剩余的一轴则垂直于显示屏。运动参数包括运动方向、运动幅度和运动速度中的至少一种。移动终端利用固定参考坐标系确定的初始状态可以准确地反映出移动终端在固定参考坐标系所表示的三维空间中的初始状态。The mobile terminal can determine the initial state of the mobile terminal in three-dimensional space according to the three-dimensional fixed reference coordinate system of the mobile terminal. Wherein, if the fixed reference coordinate system is a three-dimensional reference coordinate system, including Straight three axes, where the two axes can be parallel to the display of the mobile terminal, while the remaining one axis is perpendicular to the display. The motion parameters include at least one of a moving direction, a moving range, and a moving speed. The initial state determined by the mobile terminal using the fixed reference coordinate system can accurately reflect the initial state of the mobile terminal in the three-dimensional space represented by the fixed reference coordinate system.
步骤904,根据获取的初始的传感器数据后续的传感器数据确定移动终端的后续状态。Step 904: Determine a subsequent state of the mobile terminal according to the acquired sensor data of the initial sensor data.
具体地,移动终端在确定初始状态之后,继续获取后续的传感器数据,从而根据后续的传感器数据确定移动终端的后续状态,后续状态包括移动终端的姿态状态和运动状态,其中姿态状态包括移动终端倾斜的部分、倾斜的方向以及倾斜角度等,运动状态包括运动速度、运动加速度以及运动方向等。Specifically, after determining the initial state, the mobile terminal continues to acquire subsequent sensor data, thereby determining a subsequent state of the mobile terminal according to the subsequent sensor data, where the subsequent state includes a posture state and a motion state of the mobile terminal, where the posture state includes the mobile terminal tilting The state of the movement, the direction of the inclination, and the angle of inclination, etc., the state of motion includes the speed of motion, the acceleration of motion, and the direction of motion.
步骤906,根据后续状态相对于初始状态的变化生成飞行器操控指令。 Step 906, generating an aircraft manipulation command according to a change of the subsequent state with respect to the initial state.
具体地,移动终端以初始状态为基准,将后续状态与初始状态进行比较,从而根据后续状态相对于初始状态所变化的量生成飞行器操控指令。比如移动终端初始状态为移动终端左下角倾斜15°,那么如果后续状态为移动终端左下角从倾斜15°变化为水平,那么相当于移动终端左下角朝相反方向运动了15°,此时移动终端根据变化的量来生成飞行器操控指令。Specifically, the mobile terminal compares the subsequent state with the initial state based on the initial state, thereby generating an aircraft manipulation command according to the amount that the subsequent state changes with respect to the initial state. For example, if the initial state of the mobile terminal is inclined by 15° in the lower left corner of the mobile terminal, if the subsequent state is that the lower left corner of the mobile terminal changes from the tilt 15° to the horizontal level, then the lower left corner of the mobile terminal moves in the opposite direction by 15°, and the mobile terminal is at this time. An aircraft maneuver command is generated based on the amount of change.
举例说明,再次参照图10和图11,用户按住第一触控区域时,若移动终端确定传感器所在移动终端的初始状态为水平状态,则向左挥动移动终端,那么移动终端就可以根据后续的传感器数据确定移动终端的后续状态,根据后续状态相对于初始状态的变化检测到移动终端沿着屏幕左侧的方向运动。移动终端生成的飞行器操控指令发送至飞行器之后,飞行器执行相应的动作,比如执行左移的动作,使得飞行器按照移动终端的运动而联动。For example, referring to FIG. 10 and FIG. 11 again, when the user presses and holds the first touch area, if the mobile terminal determines that the initial state of the mobile terminal where the sensor is located is a horizontal state, then the mobile terminal is swung to the left, then the mobile terminal can follow the follow-up The sensor data determines a subsequent state of the mobile terminal, and detects that the mobile terminal moves in a direction along the left side of the screen according to a change in the subsequent state with respect to the initial state. After the aircraft control command generated by the mobile terminal is transmitted to the aircraft, the aircraft performs a corresponding action, such as performing a left shifting action, so that the aircraft is linked according to the motion of the mobile terminal.
进一步地,用户继续按住第一触控区域的情况下,向右、上或者下挥动移动终端,那么移动终端就可以检测到移动终端沿着屏幕后侧、上侧或者下次的方向运动,相应的飞行器操控指令发送到飞行器之后,使得飞行器分别执行右移、前进或者后退的动作。Further, if the user continues to hold the first touch area, and the mobile terminal is swung right, up, or down, the mobile terminal can detect that the mobile terminal moves along the back side, the upper side, or the next direction of the screen. After the corresponding aircraft maneuver command is sent to the aircraft, the aircraft is caused to perform a right shifting, advancing or retreating action, respectively.
本实施例中,用户可在移动终端处于任意状态下通过对第一触控区域的 触控操作来开启传感器控制模式,移动终端则进行初始化,根据初始的传感器数据来确定初始状态,进而根据后续的传感器数据确定后续状态,根据后续状态相对于初始状态的变化生成飞行器操控指令。这样用户没有必要必须把移动终端水平放置之后才能操控飞行器,操控更方便和精准。In this embodiment, the user can pass the first touch area in the arbitrary state of the mobile terminal. The touch operation is used to turn on the sensor control mode, and the mobile terminal initializes, determines an initial state according to the initial sensor data, and then determines a subsequent state according to the subsequent sensor data, and generates an aircraft manipulation command according to the change of the subsequent state with respect to the initial state. In this way, the user does not have to place the mobile terminal horizontally to control the aircraft, and the control is more convenient and precise.
在一个实施例中,移动终端在确定移动终端的运动状态时,判断运动幅度是否超过预设阈值,若是,则执行步骤906;若否,则放弃执行步骤906。本实施例中用户可以通过快速朝一个方向挥动移动终端并慢速归位后再向同一方向挥动移动终端,使得移动终端活动连续的超同一方向的运动参数,从而可以实现持续地操控飞行器执行相同的动作。In an embodiment, when determining the motion state of the mobile terminal, the mobile terminal determines whether the motion amplitude exceeds a preset threshold, and if yes, performs step 906; if not, abandoning step 906. In this embodiment, the user can swipe the mobile terminal in one direction and slowly return to the mobile terminal in the same direction, so that the mobile terminal can continuously move the motion parameters in the same direction, so that the aircraft can be continuously operated to perform the same operation. Actions.
如图15所示,在一个实施例中,该飞行器操控方法还包括选择预设自动操控模式操控飞行器的步骤,具体包括如下步骤:As shown in FIG. 15 , in an embodiment, the aircraft control method further includes the step of selecting a preset automatic control mode to operate the aircraft, and specifically includes the following steps:
步骤1502,检测对飞行器操控界面中预设自动操控模式图标的选择指令。Step 1502: Detect a selection instruction for a preset automatic control mode icon in the aircraft control interface.
具体地,移动终端可在飞行器操控界面中显示多个预设自动操控模式图标,如图6中的图标606、608和610。用户点击某个图标则触发相应的选择指令。其中预设自动操控模式是利用预定义的参数来操控飞行器实现预定义的动作的自动操控方式。Specifically, the mobile terminal can display a plurality of preset automatic manipulation mode icons in the aircraft manipulation interface, such as icons 606, 608, and 610 in FIG. When the user clicks on an icon, the corresponding selection instruction is triggered. The preset automatic control mode is an automatic control method that uses predefined parameters to control the aircraft to implement predefined actions.
步骤1504,根据选择指令确定相应的预设自动操控模式。Step 1504: Determine a corresponding preset automatic control mode according to the selection instruction.
具体地,移动终端将选择指令所对应的预设自动操控模式图标所对应的预设自动操控模式,作为根据选择指令确定的相应的预设自动操控模式。Specifically, the mobile terminal selects a preset automatic control mode corresponding to the preset automatic control mode icon corresponding to the instruction as a corresponding preset automatic control mode determined according to the selection instruction.
步骤1506,读取确定的预设自动操控模式所关联的飞行器组合操控指令。 Step 1506, reading the determined aircraft combination manipulation command associated with the determined preset automatic control mode.
步骤1508,向飞行器发送飞行器组合操控指令,使飞行器根据飞行器组合操控指令依次执行相应的一系列动作。 Step 1508, transmitting an aircraft combination manipulation command to the aircraft, so that the aircraft sequentially performs a corresponding series of actions according to the aircraft combination manipulation command.
具体地,移动终端上存储的每种预设自动操控模式预先关联了相应的飞行器组合操控指令,移动终端读取到飞行器组合操控指令并发送至飞行器后,飞行器则会根据飞行器组合操控指令依次执行一系列动作,以操控飞行器自动地从当前状态变化到预设自动操控模式所指定的目标状态。Specifically, each preset automatic control mode stored on the mobile terminal is pre-associated with a corresponding aircraft combination control command, and after the mobile terminal reads the aircraft combined control command and sends the command to the aircraft, the aircraft sequentially executes according to the aircraft combination control command. A series of actions to control the aircraft to automatically change from the current state to the target state specified by the preset automatic steering mode.
在一个实施例中,预设自动操控模式包括原地降落模式、返回预设地点 降落模式、飞行时紧急悬停模式和跟随锁定目标飞行模式中的至少一种。In one embodiment, the preset automatic control mode includes an in-situ landing mode, and returns to a preset location. At least one of a landing mode, an in-flight emergency hover mode, and a follow-lock target flight mode.
若确定的预设自动操控模式为原地降落模式,则飞行器可在自动地依次执行停止水平方向的移动、逐渐降低飞行高度以及到达地平面后停止旋翼的一系列动作后完成原地降落的自动飞行任务。If the determined preset automatic control mode is the in-situ landing mode, the aircraft can automatically complete the in-situ landing after automatically stopping the horizontal movement, gradually reducing the flying height, and stopping the rotor after reaching a ground level. Flight mission.
若确定的预设自动操控模式为返回预设地点降落模式,则飞行器可在自动地依次执行获取预设地点坐标、飞行至预设地点坐标、停止水平方向的移动、逐渐降低飞行高度以及到达地平面后停止旋翼的一系列动作后完成返回预设地点降落的自动飞行任务。If the determined preset automatic control mode is to return to the preset location drop mode, the aircraft may automatically perform the steps of acquiring the preset location coordinates, flying to the preset location coordinates, stopping the horizontal direction, gradually reducing the flight altitude, and arriving at the place. After the plane stops the series of actions of the rotor, the automatic flight task returns to the preset position and falls.
若确定的预设自动操控模式为飞行时紧急悬停模式,则飞行器可在自动地依次执行停止水平方向的移动并保持飞行高度的一系列动作后完成飞行时紧急悬停的自动飞行任务。If the determined preset automatic control mode is the flight emergency hover mode, the aircraft may complete the automatic flight hovering emergency flight task after automatically performing a series of actions of stopping the horizontal direction movement and maintaining the flight altitude.
若确定的预设自动操控模式为跟随锁定目标飞行模式,则飞行器可在自动地依次执行获取锁定的目标、飞行至距离锁定的目标预设距离处并保持的一系列动作后完成跟随锁定目标飞行的自动飞行任务。If the determined preset automatic control mode is the follow-lock target flight mode, the aircraft may complete the follow-lock target flight after automatically performing the acquisition of the locked target, the flight to the target preset distance of the distance lock and maintaining a series of actions. Automatic flight mission.
本实施例中,用户可以通过预设自动操控模式快捷地操控飞行器,使飞行器自动完成相应的飞行任务,提高了操作便利性。其中的原地降落模式、返回预设地点降落模式和飞行时紧急悬停模式可以实现紧急避险或者飞行器回收,跟随锁定目标飞行模式可以实现飞行器锁定目标后进行自动航行,还可以实现一个用户同时操控多个飞行器。In this embodiment, the user can quickly control the aircraft by preset the automatic control mode, so that the aircraft automatically completes the corresponding flight task, thereby improving the convenience of operation. The in-situ landing mode, the returning preset landing mode and the flight emergency hover mode can realize emergency hedging or aircraft recovery. Following the locked target flight mode, the aircraft can be locked automatically after the target is locked, and one user can simultaneously Manipulate multiple aircraft.
如图16所示,在一个实施例中,提供了一种移动终端1600,移动终端1600的内部结构可对应于如图2所示的移动终端结构,下述每个模块可全部或部分通过软件、硬件或其组合来实现。As shown in FIG. 16, in one embodiment, a mobile terminal 1600 is provided. The internal structure of the mobile terminal 1600 may correspond to the mobile terminal structure as shown in FIG. 2. Each of the following modules may pass all or part of the software. , hardware or a combination thereof.
移动终端1600包括:界面显示模块1601、触控操作检测模块1602、传感器数据处理模块1603和操控指令发送模块1604。The mobile terminal 1600 includes an interface display module 1601, a touch operation detection module 1602, a sensor data processing module 1603, and a manipulation command transmission module 1604.
界面显示模块1601,用于显示飞行器操控界面。The interface display module 1601 is configured to display an aircraft manipulation interface.
具体地,移动终端上运行有飞行器操控应用,该飞行器操控应用具有操控飞行器的功能,还可以具有对飞行器拍摄的照片或者视频进行处理的功能, 这里对飞行器拍摄的照片或者视频进行处理主要包括分类、展示、向社交好友分享以及生成行进路线。移动终端具体可按照照片或者视频的拍摄时间进行排序生成行进路线,还可以将拍摄照片或者视频时记录的地理位置信息按照相应的拍摄时间进行排序生成行进路线。这里的行进路线可以体现飞行器的行进路线,也可以进一步体现用户的行进路线。Specifically, the mobile terminal runs an aircraft control application, and the aircraft control application has the function of manipulating the aircraft, and may also have a function of processing photos or videos taken by the aircraft. The processing of photos or videos taken by the aircraft here mainly includes classification, display, sharing with social friends, and generating a route of travel. The mobile terminal may specifically sort the travel route according to the shooting time of the photo or video, and may also sort the geographic location information recorded when the photo or video is taken according to the corresponding shooting time to generate a travel route. The travel route here can reflect the travel route of the aircraft, and can further reflect the travel route of the user.
界面显示模块1601通过飞行器操控应用提供用于触发飞行器操控指令的飞行器操控界面,具体可在用于展示飞行器拍摄的照片或者视频的展示页面跳转到飞行器操控界面。举例说明,移动终端运行飞行器操控应用,首先进入如图5所示的展示页面,用户在该展示页面中可以分类查看飞行器拍摄的照片或者视频并向社交好友分享,还可以展示根据飞行器拍摄的照片或者视频生成的进行路线。移动终端在检测到对飞行器操控图标502的操作时进入如图6所示的飞行器操控界面。The interface display module 1601 provides an aircraft control interface for triggering aircraft maneuver instructions through the aircraft control application, specifically to the aircraft control interface on a display page for displaying photos or videos taken by the aircraft. For example, the mobile terminal runs the aircraft control application, first enters the display page as shown in FIG. 5, in which the user can classify and view the photos or videos taken by the aircraft and share them with social friends, and can also display photos taken according to the aircraft. Or the route generated by the video. The mobile terminal enters the aircraft control interface as shown in FIG. 6 upon detecting the operation of the aircraft control icon 502.
触控操作检测模块1602,用于检测作用于飞行器操控界面的触控操作。The touch operation detecting module 1602 is configured to detect a touch operation applied to the aircraft control interface.
具体地,第一触控区域是飞行器操控界面中的特定区域,用于承受触控操作的作用。第一触控区域可以是按钮,该按钮默认为第一状态,在触控操作检测模块1602检测到触控操作时变化为第二状态,这里的状态包括形状、颜色和图案中的至少一种,比如按钮默认为凸起状态,在触控操作检测模块1602检测到触控操作之后变化为下沉状态。第一触控区域也可以是用预设标记标识出的区域,比如用虚框圈起来或者用特殊颜色标识出的区域。第一触控区域也可以不进行标识,而是通过在首次进入飞行器操控界面时的引导图示进行指示。触控操作具体可以是触摸点击操作、触摸双击操作、触摸长按操作、滑动操作以及多点触控操作,多点触控操作是基于多个触控点的操作,比如触发多个触控点后将多个触控点汇集,或者触发多个触控点后将多个触控点扩散等。触控操作作用于第一触控区域,是指触控操作的触控点在第一触控区域内。触控操作检测模块1602可实时或者定期检测作用于飞行器操控界面的触控操作。Specifically, the first touch area is a specific area in the aircraft control interface for supporting the touch operation. The first touch area may be a button, and the button defaults to a first state, and changes to a second state when the touch operation detecting module 1602 detects the touch operation, where the state includes at least one of a shape, a color, and a pattern. For example, the button is in a raised state by default, and changes to a sinking state after the touch operation detecting module 1602 detects the touch operation. The first touch area may also be an area identified by a preset mark, such as an area circled by a virtual frame or identified by a special color. The first touch area may also be unmarked, but instead indicated by a guide icon when entering the aircraft control interface for the first time. The touch operation may specifically be a touch click operation, a touch double click operation, a touch long press operation, a sliding operation, and a multi-touch operation, and the multi-touch operation is based on operations of multiple touch points, such as triggering multiple touch points. After that, multiple touch points are collected, or multiple touch points are triggered, and then multiple touch points are spread. The touch operation is applied to the first touch area, and the touch point of the touch operation is in the first touch area. The touch operation detecting module 1602 can detect the touch operation acting on the aircraft control interface in real time or periodically.
举例说明,参照图6,第一触控区域可以是位于飞行器操控界面中的区 域602,用户通过触摸体触摸第一触控区域602并保持触控点不消失,则移动终端会检测到作用于该第一触控区域602的触控操作。触摸体比如触控笔或者用户的手指。For example, referring to FIG. 6 , the first touch area may be an area located in the aircraft control interface. In the domain 602, the user touches the first touch area 602 through the touch body and keeps the touch point from disappearing, and the mobile terminal detects the touch operation on the first touch area 602. A touch body such as a stylus or a user's finger.
传感器数据处理模块1603,用于若检测到触控操作,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令。The sensor data processing module 1603 is configured to acquire sensor data if a touch operation is detected, and obtain an aircraft manipulation command based on at least the sensor data.
传感器数据处理模块1603具体可通过读取传感器数据的接口从相应的传感器读取传感器数据,其中传感器数据可以是多个传感器的传感器数据。在一个实施例中,传感器数据来自于方向传感器、重力传感器、加速度传感器、光线传感器、电子罗盘、距离传感器、三轴陀螺仪传感器、温度传感器以及压力传感器中的至少一种。The sensor data processing module 1603 can specifically read the sensor data from the corresponding sensor through an interface that reads the sensor data, wherein the sensor data can be sensor data of the plurality of sensors. In one embodiment, the sensor data is from at least one of a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor.
传感器数据处理模块1603可根据传感器数据和飞行器操控指令的映射关系,以及获取到的传感器数据,得到飞行器操控指令。传感器数据和飞行器操控指令的映射关系可用函数来表示,该函数的自变量可以是传感器数据,因变量可以是所映射的飞行器操控指令的标识。The sensor data processing module 1603 can obtain an aircraft manipulation command according to the mapping relationship between the sensor data and the aircraft manipulation command, and the acquired sensor data. The mapping relationship between the sensor data and the aircraft maneuver command can be represented by a function, the argument of the function can be sensor data, and the dependent variable can be the identifier of the mapped aircraft maneuver instruction.
其中飞行器操控指令可以是控制飞行器飞行状态以及飞行器姿态的操控指令,也可以是控制飞行器拍摄照片或者视频的操控指令,还可以是其它用来操控飞行器执行某动作的指令。其中飞行状态比如飞行方向、飞行速度、飞行高度、悬停以及飞行目的地等中的至少一种,飞行器姿态比如侧身或者旋转等。The aircraft control command may be a control command for controlling the flight state of the aircraft and the attitude of the aircraft, or may be a control command for controlling the aircraft to take a photo or video, or may be other instructions for controlling the aircraft to perform an action. The flight state such as at least one of a flight direction, a flight speed, a flying height, a hover, and a flight destination, the attitude of the aircraft such as a side body or a rotation.
举例说明,若传感器数据为来自于压力传感器的压力数值,或者为来自于温度传感器的温度数值,或者为来自于光线传感器的光亮度值,则可根据传感器数据得到用于控制飞行器飞行速度的飞行器操控指令,比如压力数值越大飞行器飞行越快,或者温度数值越大飞行器飞行越快。若传感器数据为来自于距离传感器的距离值,则可根据传感器数据得到用于在距离值小于第一预设值时减速且在小于第二预设值时停止前进的飞行器操控指令,其中第一预设值大于第二预设值。For example, if the sensor data is a pressure value from a pressure sensor, or a temperature value from a temperature sensor, or a lightness value from a light sensor, an aircraft for controlling the flight speed of the aircraft can be obtained based on the sensor data. Manipulating commands, such as the higher the pressure value, the faster the aircraft flies, or the higher the temperature, the faster the aircraft flies. If the sensor data is a distance value from the distance sensor, an aircraft control command for decelerating when the distance value is less than the first preset value and stopping when the distance value is less than the second preset value may be obtained according to the sensor data, where the first The preset value is greater than the second preset value.
操控指令发送模块1604,用于向飞行器发送飞行器操控指令。 The command transmission module 1604 is configured to send an aircraft control command to the aircraft.
具体地,操控指令发送模块1604将得到的飞行器操控指令通过与飞行器的无线连接发送给飞行器,使得飞行器接收到飞行器操控指令后执行飞行器操控指令所指定的动作。飞行器若接收到多个飞行器操控指令,则可按照接收顺序依次执行各飞行器操控指令所指定的动作。Specifically, the manipulation command transmitting module 1604 transmits the obtained aircraft manipulation command to the aircraft through a wireless connection with the aircraft, so that the aircraft performs the action specified by the aircraft manipulation command after receiving the aircraft manipulation command. If the aircraft receives a plurality of aircraft maneuver commands, the actions specified by the respective aircraft maneuver commands may be sequentially executed in the order of reception.
上述移动终端1600,显示飞行器操控界面,该飞行器操控界面具有第一触控区域,若检测到作用于第一触控区域的触控操作时,利用传感器数据来生成飞行器操控指令发送给飞行器。这样用户在通过触控操作作用于第一触控区域时,便可以通过改变传感器所检测到的传感器数据来实现对飞行器的操控,提供了一种简单而且全新的操控方式,使得用户在操控飞行器时有更多的选择,对飞行器的操控更加方便。The mobile terminal 1600 displays an aircraft control interface. The aircraft control interface has a first touch area. When a touch operation is applied to the first touch area, the sensor data is used to generate an aircraft control command and sent to the aircraft. In this way, when the user acts on the first touch area through the touch operation, the user can control the aircraft by changing the sensor data detected by the sensor, and provides a simple and brand-new control mode, so that the user is manipulating the aircraft. There are more choices and it is more convenient to control the aircraft.
在一个实施例中,传感器数据处理模块1603具体用于若检测到作用于飞行器操控界面中第一触控区域的用于开启传感器控制模式的第一触控操作,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至检测到作用于第一触控区域的第二触控操作时停止。In one embodiment, the sensor data processing module 1603 is specifically configured to acquire sensor data when detecting a first touch operation for opening the sensor control mode in the first touch area of the aircraft control interface, and at least according to The sensor data is obtained by the aircraft control command until the second touch operation acting on the first touch area is detected.
具体地,传感器数据处理模块1603检测的触控操作包括用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作。传感器控制模式是指通过传感器数据来操控飞行器的模式,传感器数据处理模块1603在开启传感器控制模式后获取传感器数据并至少根据传感器数据得到飞行器操控指令,并将飞行器操控指令发送到飞行器。传感器数据处理模块1603在关闭传感器控制模式后将不再获取传感器数据,或者不再至少根据传感器数据得到飞行器操控指令,或者不再将飞行器操控指令发送到飞行器,而是可以通过其它方式操控飞行器,比如通过模拟摇杆操控飞行器。Specifically, the touch operation detected by the sensor data processing module 1603 includes a first touch operation for turning on the sensor control mode and a second touch operation for turning off the sensor control mode. The sensor control mode refers to a mode in which the aircraft is manipulated by sensor data. The sensor data processing module 1603 acquires sensor data after turning on the sensor control mode and obtains an aircraft control command based on at least the sensor data, and transmits the aircraft control command to the aircraft. The sensor data processing module 1603 will no longer acquire the sensor data after the sensor control mode is turned off, or no longer at least obtain the aircraft control command according to the sensor data, or no longer send the aircraft control command to the aircraft, but can manipulate the aircraft by other means. For example, the aircraft is controlled by an analog joystick.
本实施例中,通过分别用于开启和关闭传感器控制模式的触控操作,可以灵活地控制进入传感器控制模式的时机,从而在传感器控制模式下利用传感器所检测到的传感器数据的变化来操控飞行器,对飞行器的操控更加便捷。In this embodiment, the timing of entering the sensor control mode can be flexibly controlled by the touch operation for turning the sensor control mode on and off, respectively, thereby using the change of the sensor data detected by the sensor to control the aircraft in the sensor control mode. The handling of the aircraft is more convenient.
在一个实施例中,用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作可以相同。此时触控操作可从触摸点击操作、 触摸双击操作、滑动操作以及多点触控操作中选择。In one embodiment, the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be the same. At this time, the touch operation can be performed from a touch click operation, Touch double-click, slide, and multi-touch to select.
比如若检测到对第一触控区域的一次触摸点击操作,则开启传感器控制模式,进而获取传感器数据,并至少根据传感器数据得到飞行器操控指令,向飞行器发送飞行器操控指令。若再次检测到对第一触控区域的一次触摸点击操作,则关闭传感器控制模式。For example, if a touch click operation on the first touch area is detected, the sensor control mode is turned on, and the sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the aircraft control command is sent to the aircraft. If a touch click operation on the first touch area is detected again, the sensor control mode is turned off.
在一个实施例中,用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作可以不相同。此时两种触控操作可分别从触摸点击操作、触摸双击操作、滑动操作以及多点触控操作中选择。In one embodiment, the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be different. At this time, the two touch operations can be selected from a touch click operation, a touch double click operation, a slide operation, and a multi-touch operation, respectively.
比如若检测到对第一触控区域的触摸点击操作,则开启传感器控制模式,进而获取传感器数据,并至少根据传感器数据得到飞行器操控指令,向飞行器发送飞行器操控指令。若检测到对第一触控区域的触摸双击操作,则关闭传感器控制模式。For example, if a touch click operation on the first touch area is detected, the sensor control mode is turned on, and sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data, and the aircraft control command is sent to the aircraft. If a touch double click operation on the first touch area is detected, the sensor control mode is turned off.
在一个实施例中,用于开启传感器控制模式的第一触控操作和用于关闭传感器控制模式的第二触控操作可以包含于一个组合触控操作中。组合触控操作比如触摸长按操作,包括触发触摸长按操作的触控操作和解除触摸长按操作的触控操作。In one embodiment, the first touch operation for turning on the sensor control mode and the second touch operation for turning off the sensor control mode may be included in one combined touch operation. The combined touch operation, such as a touch long press operation, includes a touch operation that triggers a long press operation and a touch operation that releases a long press operation.
在一个实施例中,传感器数据处理模块1603具体用于自检测到第三触控操作起开始计时,若计时达到预设时长且第三触控操作保持作用于飞行器操控界面中的第一触控区域,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至第三触控操作停止。In one embodiment, the sensor data processing module 1603 is specifically configured to start timing when the third touch operation is detected, if the timing reaches a preset duration and the third touch operation remains to act on the first touch in the aircraft control interface. For the area, the sensor data is acquired, and at least the aircraft control command is obtained according to the sensor data until the third touch operation is stopped.
具体地,本实施例中检测的触控操作为持续触控操作,传感器数据处理模块1603在检测到该触控操作后,在该触控操作对第一触控区域的所用时间内,获取传感器数据,并至少根据传感器数据得到飞行器操控指令,以及向飞行器发送飞行器操控指令,直至触控点对第一触控区域的作用消失。其中触控操作的作用时间是指从检测到该触控操作的时刻到该触控操作消失的时间段。Specifically, the touch operation detected in the embodiment is a continuous touch operation, and after detecting the touch operation, the sensor data processing module 1603 acquires a sensor during the use time of the touch operation on the first touch area. Data, and at least according to the sensor data, obtain an aircraft control command, and send an aircraft control command to the aircraft until the effect of the touch point on the first touch area disappears. The action time of the touch operation refers to a time period from when the touch operation is detected to when the touch operation disappears.
其中,预设时长是为了与点触操作区分,若检测到触控点起的预设时长 之内该触控点消失,则识别为点触操作,若达到预设时长触控点仍未消失,则识别为需要检测的持续的触控操作,进入传感器控制模式。自检测到第三触控操作的触控点起开始计时并计时达到预设时长,是用于开启传感器控制模式的第一触控操作,触控点对第一触控区域的作用消失则是用于关闭传感器控制模式的第二触控操作。The preset duration is for distinguishing from the touch operation, and the preset duration from the touch point is detected. After the touch point disappears, it is recognized as a touch operation. If the touch point has not disappeared after reaching the preset time, it is recognized as a continuous touch operation that needs to be detected, and enters the sensor control mode. The first touch operation for turning on the sensor control mode is started when the touch point of the third touch operation is detected and the time is up to the preset time. The effect of the touch point on the first touch area disappears. A second touch operation for turning off the sensor control mode.
本实施例中,在检测到触控点起开始计时,若达到预设时长触控点仍保持作用于第一触控区域,可防止因用户误触第一触控区域而造成飞行器失控。In this embodiment, when the touch point is detected, the time is started. If the touch time is still applied to the first touch area when the preset time is reached, the aircraft may be prevented from being out of control due to the user accidentally touching the first touch area.
在其它实施例中,传感器数据处理模块1603也可在检测到触控操作之后立即获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至触控点对第一触控区域的作用消失。In other embodiments, the sensor data processing module 1603 may also acquire sensor data immediately after detecting the touch operation, and at least obtain an aircraft manipulation command according to the sensor data until the effect of the touch point on the first touch area disappears.
在一个实施例中,传感器数据处理模块1603具体用于检测作用于飞行器操控界面中第二触控区域一触控按钮的按压触摸操作,检测到时,获取传感器数据;检测触控按钮跟随按压触摸操作在第二触控区域或飞行器操控界面中的移动,根据移动获取模拟摇杆操控指令;根据传感器数据以及模拟摇杆操控指令得到飞行器操控指令。In one embodiment, the sensor data processing module 1603 is specifically configured to detect a touch touch operation of a touch button applied to the second touch area of the aircraft control interface. When detected, the sensor data is acquired; and the touch button is detected to follow the touch touch. The operation is operated in the second touch area or the aircraft control interface, and the analog joystick manipulation command is acquired according to the movement; the aircraft manipulation command is obtained according to the sensor data and the analog joystick manipulation command.
如图17所示,在一个实施例中,移动终端1600还包括:触摸操作检测模块1605、模拟摇杆操控指令获取模块1606和模拟摇杆操控指令发送模块1607。As shown in FIG. 17, in one embodiment, the mobile terminal 1600 further includes a touch operation detection module 1605, an analog joystick manipulation command acquisition module 1606, and an analog joystick manipulation command transmission module 1607.
触摸操作检测模块1605,用于检测作用于飞行器操控界面中第二触控区域的触摸操作。第二触控区域用于模拟摇杆操作。The touch operation detecting module 1605 is configured to detect a touch operation applied to the second touch area in the aircraft control interface. The second touch area is used to simulate the joystick operation.
具体地,第二触控区域是飞行器操控界面中的特定区域,用于承受触摸操作来模拟摇杆操作。触摸操作比如触摸点击操作、触摸双击操作、触摸长按操作、滑动操作以及多点触控操作。作用于第二触控区域的触摸操作与作用于第一触控区域的触控操作分别实现不同的操控方式。Specifically, the second touch area is a specific area in the aircraft manipulation interface for withstanding a touch operation to simulate a joystick operation. Touch operations such as touch click operations, touch double tap operations, touch long press operations, swipe operations, and multi-touch operations. The touch operation applied to the second touch area and the touch operation applied to the first touch area respectively implement different control modes.
在一个实施例中,第二触控区域可以包围第一触控区域,此时第二触控区域与第一触控区域不重叠,触摸操作与检测的触控操作可以存在相同的情况。在其它实施例中,第二触控区域可与第一触控区域相分离。 In one embodiment, the second touch area can surround the first touch area. The second touch area does not overlap with the first touch area. The touch operation and the detected touch operation may be the same. In other embodiments, the second touch area can be separated from the first touch area.
模拟摇杆操控指令获取模块1606,用于获取触摸操作所触发的模拟摇杆操控指令。The analog joystick manipulation command acquisition module 1606 is configured to acquire an analog joystick manipulation command triggered by the touch operation.
模拟摇杆操控指令发送模块1607,用于向飞行器发送模拟摇杆操控指令。The analog joystick manipulation command sending module 1607 is configured to send an analog joystick manipulation command to the aircraft.
具体地,触摸操作作用于第二触控区域的不同区域,可分别触发不同的模拟摇杆操控指令。具体第二触控区域中可定义四个主方向,比如上下左右,从而模拟摇杆操控指令获取模块1606可根据触摸操作作用于第二触控区域中相对于四个主方向的相对位置来触发相应的模拟摇杆操控指令。模拟摇杆操控指令与飞行器操控指令不冲突。优选地,模拟摇杆操控指令用于操控飞行器垂直升降和飞行器姿态的变化,飞行器操控指令用于操控飞行器沿水平面的各方向的移动。Specifically, the touch operation acts on different regions of the second touch area, and different analog joystick manipulation commands can be triggered respectively. Four main directions may be defined in the second touch area, such as up, down, left and right, so that the analog rocker manipulation command acquisition module 1606 can be triggered according to the relative position of the second touch region relative to the four main directions according to the touch operation. The corresponding analog joystick control command. The analog joystick control command does not conflict with the aircraft control command. Preferably, the analog rocker steering command is used to manipulate the vertical movement of the aircraft and the change in attitude of the aircraft, and the aircraft maneuver command is used to manipulate the movement of the aircraft in various directions along the horizontal plane.
参照图8,若触摸操作的触控点作用于第二触控区域801的主方向上,如图8中四个手势802、803、804以及805所表示的触摸操作,则移动终端可触发该主方向所对应的模拟摇杆操控指令,将模拟摇杆操控指令发送到飞行器之后,飞行器可根据接收到的模拟摇杆操控指令实施上升、下降、左旋或者右旋的动作。Referring to FIG. 8 , if the touch point of the touch operation acts on the main direction of the second touch area 801, as shown by the four gestures 802, 803, 804, and 805 in FIG. 8 , the mobile terminal may trigger the touch operation. After the analog joystick manipulation command corresponding to the main direction is sent to the aircraft, the aircraft can perform the ascending, descending, left-handed or right-handed motion according to the received analog joystick manipulation command.
若触摸操作作用于第二触控区域中主方向之外的位置,则模拟摇杆操控指令获取模块1606可根据触摸操作的触控点映射在主方向上的分量来触发相应的组合的模拟摇杆操控指令,模拟摇杆操控指令发送模块1607将组合的模拟摇杆操控指令发送到飞行器,飞行器可根据接收到的组合的模拟摇杆操控指令实施左旋上升、右旋上升、左旋下降或者右旋下降的动作。If the touch operation is applied to a position other than the main direction in the second touch area, the analog joystick manipulation instruction acquisition module 1606 can trigger the corresponding combined analog shake according to the component of the touch operation map of the touch operation in the main direction. The lever manipulation command, the analog joystick manipulation command sending module 1607 sends the combined analog joystick manipulation command to the aircraft, and the aircraft can perform a left-handed rise, a right-handed rise, a left-handed fall, or a right-handed according to the received combined analog joystick manipulation command. The action of falling.
本实施例中,检测作用于飞行器操控界面的触控操作,并检测作用于飞行器操控界面的第二触控区域的触摸操作,从而根据不同的检测结果的组合来实现飞行器的不同的操控方式。这样使得飞行器的操控方式更加多样化,对飞行器的操控更加灵活、方便。In this embodiment, the touch operation applied to the control interface of the aircraft is detected, and the touch operation of the second touch area acting on the control interface of the aircraft is detected, so that different control modes of the aircraft are implemented according to a combination of different detection results. This makes the aircraft's control mode more diverse, and the handling of the aircraft is more flexible and convenient.
在一个实施例中,传感器数据处理模块1603具体用于若检测到第四触控操作的触控点作用于第一触控区域,则获取传感器数据,并至少根据传感器数据得到飞行器操控指令,直至触控点消失时停止;移动终端1600还包括摇 杆操控模拟模块(图中未示出),用于当触控点移动到飞行器操控界面中的第二触控区域时,根据触控点在第二触控区域中的位置触发模拟摇杆操控指令并发送到飞行器;第二触控区域用于模拟摇杆操作。其中摇杆操控模拟模块可以包括上述触摸操作检测模块1605、模拟摇杆操控指令获取模块1606和模拟摇杆操控指令发送模块1607。In one embodiment, the sensor data processing module 1603 is specifically configured to: if the touch point of the fourth touch operation is detected to act on the first touch area, acquire sensor data, and obtain an aircraft control command according to at least the sensor data; Stopping when the touch point disappears; the mobile terminal 1600 also includes shaking The lever control simulation module (not shown) is configured to trigger the analog joystick control according to the position of the touch point in the second touch area when the touch point moves to the second touch area in the aircraft control interface The command is sent to the aircraft; the second touch area is used to simulate the joystick operation. The joystick manipulation simulation module may include the above-described touch operation detection module 1605, an analog joystick manipulation instruction acquisition module 1606, and an analog joystick manipulation command transmission module 1607.
如图18所示,在一个实施例中,传感器数据处理模块1603包括:初始状态确定模块1603a、后续状态确定模块1603b和飞行器操控指令生成模块1603c。As shown in FIG. 18, in one embodiment, the sensor data processing module 1603 includes an initial state determination module 1603a, a subsequent state determination module 1603b, and an aircraft manipulation command generation module 1603c.
初始状态确定模块1603a,用于根据获取的初始的传感器数据确定传感器所在移动终端的初始状态。The initial state determining module 1603a is configured to determine an initial state of the mobile terminal where the sensor is located according to the obtained initial sensor data.
具体地,传感器数据包括用于反映移动终端的姿态和运动中的至少一种的数据。初始的传感器数据是移动终端在进入传感器控制模式之后最初收到的传感器数据,用来确定移动终端当前所处的状态,定义为初始状态。初始状态包括移动终端的姿态状态和运动状态,其中姿态状态包括移动终端倾斜的部分、倾斜的方向以及倾斜角度等,运动状态包括运动速度、运动加速度以及运动方向等。Specifically, the sensor data includes data for reflecting at least one of a posture and a motion of the mobile terminal. The initial sensor data is the sensor data initially received by the mobile terminal after entering the sensor control mode, and is used to determine the current state of the mobile terminal, which is defined as an initial state. The initial state includes an attitude state and a motion state of the mobile terminal, wherein the posture state includes a tilted portion of the mobile terminal, a tilted direction, and a tilt angle, and the like, and the motion state includes a motion speed, a motion acceleration, and a motion direction.
初始状态确定模块1603a可根据移动终端的三维固定参考坐标系确定移动终端在三维空间中的初始状态。其中,若固定参考坐标系为三维参考坐标系,包括相互垂直的三轴,其中两轴可以平行于移动终端的显示屏,而剩余的一轴则垂直于显示屏。运动参数包括运动方向、运动幅度和运动速度中的至少一种。移动终端利用固定参考坐标系确定的初始状态可以准确地反映出移动终端在固定参考坐标系所表示的三维空间中的初始状态。The initial state determination module 1603a may determine an initial state of the mobile terminal in three-dimensional space according to a three-dimensional fixed reference coordinate system of the mobile terminal. Wherein, if the fixed reference coordinate system is a three-dimensional reference coordinate system, including three axes perpendicular to each other, two axes may be parallel to the display screen of the mobile terminal, and the remaining one axis is perpendicular to the display screen. The motion parameters include at least one of a moving direction, a moving range, and a moving speed. The initial state determined by the mobile terminal using the fixed reference coordinate system can accurately reflect the initial state of the mobile terminal in the three-dimensional space represented by the fixed reference coordinate system.
后续状态确定模块1603b,用于根据获取的初始的传感器数据后续的传感器数据确定移动终端的后续状态。The subsequent state determining module 1603b is configured to determine a subsequent state of the mobile terminal according to the acquired sensor data subsequent to the sensor data.
具体地,在确定初始状态之后,后续状态确定模块1603b继续获取后续的传感器数据,从而根据后续的传感器数据确定移动终端的后续状态,后续状态包括移动终端的姿态状态和运动状态,其中姿态状态包括移动终端倾斜 的部分、倾斜的方向以及倾斜角度等,运动状态包括运动速度、运动加速度以及运动方向等。Specifically, after determining the initial state, the subsequent state determining module 1603b continues to acquire subsequent sensor data, thereby determining a subsequent state of the mobile terminal according to the subsequent sensor data, where the subsequent state includes a posture state and a motion state of the mobile terminal, where the posture state includes Mobile terminal tilt The state of the movement, the direction of the inclination, and the angle of inclination, etc., the state of motion includes the speed of motion, the acceleration of motion, and the direction of motion.
飞行器操控指令生成模块1603c,用于根据后续状态相对于初始状态的变化生成飞行器操控指令。The aircraft maneuver instruction generation module 1603c is configured to generate an aircraft maneuver instruction according to a change of the subsequent state with respect to the initial state.
具体地,飞行器操控指令生成模块1603c以初始状态为基准,将后续状态与初始状态进行比较,从而根据后续状态相对于初始状态所变化的量生成飞行器操控指令。比如移动终端初始状态为移动终端左下角倾斜15°,那么如果后续状态为移动终端左下角从倾斜15°变化为水平,那么相当于移动终端左下角朝相反方向运动了15°,此时移动终端根据变化的量来生成飞行器操控指令。Specifically, the aircraft manipulation command generation module 1603c compares the subsequent state with the initial state based on the initial state, thereby generating an aircraft manipulation command according to the amount of change of the subsequent state with respect to the initial state. For example, if the initial state of the mobile terminal is inclined by 15° in the lower left corner of the mobile terminal, if the subsequent state is that the lower left corner of the mobile terminal changes from the tilt 15° to the horizontal level, then the lower left corner of the mobile terminal moves in the opposite direction by 15°, and the mobile terminal is at this time. An aircraft maneuver command is generated based on the amount of change.
本实施例中,用户可在移动终端处于任意状态下通过对第一触控区域的触控操作来开启传感器控制模式,移动终端则进行初始化,根据初始的传感器数据来确定初始状态,进而根据后续的传感器数据确定后续状态,根据后续状态相对于初始状态的变化生成飞行器操控指令。这样用户没有必要必须把移动终端水平放置之后才能操控飞行器,操控更方便和精准。In this embodiment, the user can turn on the sensor control mode by using the touch operation on the first touch area in the arbitrary state of the mobile terminal, and the mobile terminal initializes the initial state according to the initial sensor data, and then according to the subsequent The sensor data determines a subsequent state, and an aircraft maneuver command is generated based on a change in the subsequent state relative to the initial state. In this way, the user does not have to place the mobile terminal horizontally to control the aircraft, and the control is more convenient and precise.
在一个实施例中,传感器数据来自于方向传感器、重力传感器、加速度传感器、光线传感器、电子罗盘、距离传感器、三轴陀螺仪传感器、温度传感器以及压力传感器中的至少一种。In one embodiment, the sensor data is from at least one of a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor.
如图19所示,在一个实施例中,移动终端1600还包括:预设自动操控模式确定模块1608、飞行器组合操控指令读取模块1609和飞行器组合操控指令发送模块1610。As shown in FIG. 19, in one embodiment, the mobile terminal 1600 further includes: a preset automatic steering mode determining module 1608, an aircraft combination steering command reading module 1609, and an aircraft combination steering command transmitting module 1610.
预设自动操控模式确定模块1608,用于检测对飞行器操控界面中预设自动操控模式图标的选择指令;根据选择指令确定相应的预设自动操控模式。The preset automatic control mode determining module 1608 is configured to detect a selection instruction for the preset automatic control mode icon in the aircraft control interface; and determine a corresponding preset automatic control mode according to the selection instruction.
具体地,预设自动操控模式确定模块1608可在飞行器操控界面中显示多个预设自动操控模式图标,如图6中的图标606、608和610。用户点击某个图标则触发相应的选择指令。其中预设自动操控模式是利用预定义的参数来操控飞行器实现预定义的动作的自动操控方式。将选择指令所对应的预设自 动操控模式图标所对应的预设自动操控模式,作为根据选择指令确定的相应的预设自动操控模式。Specifically, the preset automatic manipulation mode determination module 1608 can display a plurality of preset automatic manipulation mode icons in the aircraft manipulation interface, such as icons 606, 608, and 610 in FIG. When the user clicks on an icon, the corresponding selection instruction is triggered. The preset automatic control mode is an automatic control method that uses predefined parameters to control the aircraft to implement predefined actions. The preset corresponding to the selection instruction will be The preset automatic control mode corresponding to the motion control mode icon is used as a corresponding preset automatic control mode determined according to the selection instruction.
飞行器组合操控指令读取模块1609,用于读取确定的预设自动操控模式所关联的飞行器组合操控指令。The aircraft combination manipulation command reading module 1609 is configured to read the aircraft combination manipulation command associated with the determined preset automatic control mode.
飞行器组合操控指令发送模块1610,用于向飞行器发送飞行器组合操控指令,使飞行器根据飞行器组合操控指令依次执行相应的一系列动作。The aircraft combination command transmission module 1610 is configured to send an aircraft combination manipulation command to the aircraft, so that the aircraft sequentially performs a corresponding series of actions according to the aircraft combination manipulation command.
具体地,移动终端上存储的每种预设自动操控模式预先关联了相应的飞行器组合操控指令,飞行器组合操控指令读取模块1609读取到飞行器组合操控指令并由飞行器组合操控指令发送模块1610发送至飞行器后,飞行器则会根据飞行器组合操控指令依次执行一系列动作,以操控飞行器自动地从当前状态变化到预设自动操控模式所指定的目标状态。Specifically, each preset automatic control mode stored on the mobile terminal is pre-associated with a corresponding aircraft combination manipulation command, and the aircraft combination manipulation command reading module 1609 reads the aircraft combination manipulation command and is transmitted by the aircraft combination manipulation command transmission module 1610. After the aircraft, the aircraft will perform a series of actions according to the aircraft combination control command to control the aircraft to automatically change from the current state to the target state specified by the preset automatic control mode.
在一个实施例中,预设自动操控模式包括原地降落模式、返回预设地点降落模式、飞行时紧急悬停模式和跟随锁定目标飞行模式中的至少一种。In one embodiment, the preset automatic control mode includes at least one of an in situ landing mode, a return preset landing mode, an in-flight emergency hover mode, and a follow-lock target flight mode.
若确定的预设自动操控模式为原地降落模式,则飞行器可在自动地依次执行停止水平方向的移动、逐渐降低飞行高度以及到达地平面后停止旋翼的一系列动作后完成原地降落的自动飞行任务。If the determined preset automatic control mode is the in-situ landing mode, the aircraft can automatically complete the in-situ landing after automatically stopping the horizontal movement, gradually reducing the flying height, and stopping the rotor after reaching a ground level. Flight mission.
若确定的预设自动操控模式为返回预设地点降落模式,则飞行器可在自动地依次执行获取预设地点坐标、飞行至预设地点坐标、停止水平方向的移动、逐渐降低飞行高度以及到达地平面后停止旋翼的一系列动作后完成返回预设地点降落的自动飞行任务。If the determined preset automatic control mode is to return to the preset location drop mode, the aircraft may automatically perform the steps of acquiring the preset location coordinates, flying to the preset location coordinates, stopping the horizontal direction, gradually reducing the flight altitude, and arriving at the place. After the plane stops the series of actions of the rotor, the automatic flight task returns to the preset position and falls.
若确定的预设自动操控模式为飞行时紧急悬停模式,则飞行器可在自动地依次执行停止水平方向的移动并保持飞行高度的一系列动作后完成飞行时紧急悬停的自动飞行任务。If the determined preset automatic control mode is the flight emergency hover mode, the aircraft may complete the automatic flight hovering emergency flight task after automatically performing a series of actions of stopping the horizontal direction movement and maintaining the flight altitude.
若确定的预设自动操控模式为跟随锁定目标飞行模式,则飞行器可在自动地依次执行获取锁定的目标、飞行至距离锁定的目标预设距离处并保持的一系列动作后完成跟随锁定目标飞行的自动飞行任务。If the determined preset automatic control mode is the follow-lock target flight mode, the aircraft may complete the follow-lock target flight after automatically performing the acquisition of the locked target, the flight to the target preset distance of the distance lock and maintaining a series of actions. Automatic flight mission.
本实施例中,用户可以通过预设自动操控模式快捷地操控飞行器,使飞 行器自动完成相应的飞行任务,提高了操作便利性。其中的原地降落模式、返回预设地点降落模式和飞行时紧急悬停模式可以实现紧急避险或者飞行器回收,跟随锁定目标飞行模式可以实现飞行器锁定目标后进行自动航行,还可以实现一个用户同时操控多个飞行器。In this embodiment, the user can quickly control the aircraft by using a preset automatic control mode to make the fly The line automatically completes the corresponding flight task, which improves the convenience of operation. The in-situ landing mode, the returning preset landing mode and the flight emergency hover mode can realize emergency hedging or aircraft recovery. Following the locked target flight mode, the aircraft can be locked automatically after the target is locked, and one user can simultaneously Manipulate multiple aircraft.
本领域普通技术人员可以理解实现上述实施例方法中的全部或部分流程,是可以通过计算机程序来指令相关的硬件来完成,所述的程序可存储于一计算机可读取存储介质中,该程序在执行时,可包括如上述各方法的实施例的流程。其中,所述的存储介质可为磁碟、光盘、只读存储记忆体(Read-Only Memory,ROM)等非易失性存储介质,或随机存储记忆体(Random Access Memory,RAM)等。One of ordinary skill in the art can understand that all or part of the process of implementing the foregoing embodiments can be completed by a computer program to instruct related hardware, and the program can be stored in a computer readable storage medium. When executed, the flow of an embodiment of the methods as described above may be included. The storage medium may be a non-volatile storage medium such as a magnetic disk, an optical disk, a read-only memory (ROM), or a random access memory (RAM).
以上所述实施例的各技术特征可以进行任意的组合,为使描述简洁,未对上述实施例中的各个技术特征所有可能的组合都进行描述,然而,只要这些技术特征的组合不存在矛盾,都应当认为是本说明书记载的范围。The technical features of the above-described embodiments may be arbitrarily combined. For the sake of brevity of description, all possible combinations of the technical features in the above embodiments are not described. However, as long as there is no contradiction between the combinations of these technical features, All should be considered as the scope of this manual.
以上所述实施例仅表达了本发明的几种实施方式,其描述较为具体和详细,但并不能因此而理解为对发明专利范围的限制。应当指出的是,对于本领域的普通技术人员来说,在不脱离本发明构思的前提下,还可以做出若干变形和改进,这些都属于本发明的保护范围。因此,本发明专利的保护范围应以所附权利要求为准。 The above-described embodiments are merely illustrative of several embodiments of the present invention, and the description thereof is more specific and detailed, but is not to be construed as limiting the scope of the invention. It should be noted that a number of variations and modifications may be made by those skilled in the art without departing from the spirit and scope of the invention. Therefore, the scope of the invention should be determined by the appended claims.

Claims (20)

  1. 一种飞行器操控方法,包括:An aircraft handling method includes:
    显示飞行器操控界面;Display the aircraft control interface;
    检测作用于所述飞行器操控界面的触控操作;Detecting a touch operation acting on the aircraft control interface;
    若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令;及If the touch operation is detected, acquiring sensor data, and obtaining an aircraft manipulation command based on at least the sensor data; and
    向飞行器发送所述飞行器操控指令。The aircraft maneuver command is sent to the aircraft.
  2. 根据权利要求1所述的方法,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The method according to claim 1, wherein if the touch operation is detected, acquiring sensor data, and obtaining the aircraft manipulation command based on at least the sensor data comprises:
    若检测到作用于所述飞行器操控界面中第一触控区域的用于开启传感器控制模式的第一触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至检测到作用于所述第一触控区域的第二触控操作时停止。If the first touch operation for opening the sensor control mode is detected in the first touch area of the aircraft control interface, acquiring sensor data, and obtaining an aircraft control command according to at least the sensor data, until the detection is detected. The second touch operation applied to the first touch area is stopped.
  3. 根据权利要求1所述的方法,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The method according to claim 1, wherein if the touch operation is detected, acquiring sensor data, and obtaining the aircraft manipulation command based on at least the sensor data comprises:
    自检测到第三触控操作起开始计时,若计时达到预设时长且所述第三触控操作保持作用于所述飞行器操控界面中的第一触控区域,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至所述第三触控操作停止。Starting from the detection of the third touch operation, if the timing reaches a preset duration and the third touch operation remains applied to the first touch area in the aircraft control interface, the sensor data is acquired, and at least according to The sensor data is obtained by the aircraft control command until the third touch operation is stopped.
  4. 根据权利要求1所述的方法,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The method according to claim 1, wherein if the touch operation is detected, acquiring sensor data, and obtaining the aircraft manipulation command based on at least the sensor data comprises:
    检测作用于所述飞行器操控界面中第二触控区域一触控按钮的按压触摸操作,检测到时,获取传感器数据;Detecting a pressing touch operation of a touch button acting on the second touch area of the aircraft control interface, and acquiring sensor data when detecting;
    检测所述触控按钮跟随所述按压触摸操作在所述第二触控区域或所述飞 行器操控界面中的移动,根据所述移动获取模拟摇杆操控指令;及Detecting the touch button following the pressing touch operation in the second touch area or the fly a movement in the console control interface to obtain an analog joystick manipulation command based on the movement; and
    根据所述传感器数据以及模拟摇杆操控指令得到飞行器操控指令。An aircraft maneuver command is obtained based on the sensor data and an analog joystick manipulation command.
  5. 根据权利要求1所述的方法,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The method according to claim 1, wherein if the touch operation is detected, acquiring sensor data, and obtaining the aircraft manipulation command based on at least the sensor data comprises:
    若检测到第四触控操作的触控点作用于所述飞行器操控界面中的第一触控区域,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至所述触控点消失时停止;If it is detected that the touch point of the fourth touch operation acts on the first touch area in the aircraft control interface, acquiring sensor data, and obtaining an aircraft control command according to at least the sensor data, until the touch point Stop when disappearing;
    所述方法还包括:The method further includes:
    当所述触控点移动到所述飞行器操控界面中的第二触控区域时,根据所述触控点在所述第二触控区域中的位置触发模拟摇杆操控指令并发送到所述飞行器;所述第二触控区域用于模拟摇杆操作。When the touch point moves to the second touch area in the aircraft control interface, triggering an analog joystick manipulation command according to the position of the touch point in the second touch area and transmitting to the The aircraft; the second touch area is used to simulate a joystick operation.
  6. 根据权利要求1所述的方法,其特征在于,所述至少根据所述传感器数据得到飞行器操控指令包括:The method of claim 1 wherein said obtaining aircraft control commands based on at least said sensor data comprises:
    根据获取的初始的传感器数据确定传感器所在移动终端的初始状态;Determining an initial state of the mobile terminal where the sensor is located according to the obtained initial sensor data;
    根据获取的初始的传感器数据后续的传感器数据确定所述移动终端的后续状态;及Determining a subsequent state of the mobile terminal according to the acquired sensor data subsequent sensor data; and
    根据所述后续状态相对于所述初始状态的变化生成飞行器操控指令。An aircraft maneuver command is generated based on the change in the subsequent state relative to the initial state.
  7. 根据权利要求1所述的方法,其特征在于,所述传感器数据来自于方向传感器、重力传感器、加速度传感器、光线传感器、电子罗盘、距离传感器、三轴陀螺仪传感器、温度传感器以及压力传感器中的至少一种。The method according to claim 1, wherein the sensor data is derived from a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor. At least one.
  8. 根据权利要求1所述的方法,其特征在于,还包括:The method of claim 1 further comprising:
    检测对所述飞行器操控界面中预设自动操控模式图标的选择指令;Detecting a selection instruction for a preset automatic control mode icon in the aircraft control interface;
    根据所述选择指令确定相应的预设自动操控模式;Determining a corresponding preset automatic control mode according to the selection instruction;
    读取确定的预设自动操控模式所关联的飞行器组合操控指令;及Reading the determined aircraft combination manipulation command associated with the determined preset automatic control mode; and
    向所述飞行器发送所述飞行器组合操控指令,使所述飞行器根据所述飞行器组合操控指令依次执行相应的一系列动作。 The aircraft combination steering command is transmitted to the aircraft to cause the aircraft to sequentially perform a corresponding series of actions in accordance with the aircraft combination steering command.
  9. 根据权利要求8所述的方法,其特征在于,所述预设自动操控模式包括原地降落模式、返回预设地点降落模式、飞行时紧急悬停模式和跟随锁定目标飞行模式中的至少一种。The method according to claim 8, wherein the preset automatic control mode comprises at least one of an in situ landing mode, a return preset landing mode, an in-flight emergency hover mode, and a follow-lock target flight mode. .
  10. 一种移动终端,包括存储器和处理器,所述存储器中储存有计算机可读指令,其特征在于,所述计算机可读指令被所述处理器执行时,使得所述处理器执行以下步骤:A mobile terminal comprising a memory and a processor, wherein the memory stores computer readable instructions, wherein when the computer readable instructions are executed by the processor, the processor performs the following steps:
    显示飞行器操控界面;Display the aircraft control interface;
    检测作用于所述飞行器操控界面的触控操作;Detecting a touch operation acting on the aircraft control interface;
    若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令;及If the touch operation is detected, acquiring sensor data, and obtaining an aircraft manipulation command based on at least the sensor data; and
    向飞行器发送所述飞行器操控指令。The aircraft maneuver command is sent to the aircraft.
  11. 根据权利要求10所述的移动终端,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The mobile terminal according to claim 10, wherein if the touch operation is detected, acquiring sensor data and obtaining an aircraft manipulation command based on at least the sensor data comprises:
    若检测到作用于所述飞行器操控界面中第一触控区域的用于开启传感器控制模式的第一触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至检测到作用于所述第一触控区域的第二触控操作时停止。If the first touch operation for opening the sensor control mode is detected in the first touch area of the aircraft control interface, acquiring sensor data, and obtaining an aircraft control command according to at least the sensor data, until the detection is detected. The second touch operation applied to the first touch area is stopped.
  12. 根据权利要求10所述的移动终端,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The mobile terminal according to claim 10, wherein if the touch operation is detected, acquiring sensor data and obtaining an aircraft manipulation command based on at least the sensor data comprises:
    自检测到第三触控操作起开始计时,若计时达到预设时长且所述第三触控操作保持作用于所述飞行器操控界面中的第一触控区域,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至所述第三触控操作停止。Starting from the detection of the third touch operation, if the timing reaches a preset duration and the third touch operation remains applied to the first touch area in the aircraft control interface, the sensor data is acquired, and at least according to The sensor data is obtained by the aircraft control command until the third touch operation is stopped.
  13. 根据权利要求10所述的移动终端,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控 指令包括:The mobile terminal according to claim 10, wherein if the touch operation is detected, sensor data is acquired, and at least the aircraft control is obtained according to the sensor data. Instructions include:
    检测作用于所述飞行器操控界面中第二触控区域一触控按钮的按压触摸操作,检测到时,获取传感器数据;Detecting a pressing touch operation of a touch button acting on the second touch area of the aircraft control interface, and acquiring sensor data when detecting;
    检测所述触控按钮跟随所述按压触摸操作在所述第二触控区域或所述飞行器操控界面中的移动,根据所述移动获取模拟摇杆操控指令;及Detecting that the touch button follows the movement of the pressing touch operation in the second touch area or the aircraft manipulation interface, and acquiring an analog joystick manipulation instruction according to the movement;
    根据所述传感器数据以及模拟摇杆操控指令得到飞行器操控指令。An aircraft maneuver command is obtained based on the sensor data and an analog joystick manipulation command.
  14. 根据权利要求10所述的移动终端,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The mobile terminal according to claim 10, wherein if the touch operation is detected, acquiring sensor data and obtaining an aircraft manipulation command based on at least the sensor data comprises:
    若检测到第四触控操作的触控点作用于所述飞行器操控界面中的第一触控区域,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至所述触控点消失时停止;If it is detected that the touch point of the fourth touch operation acts on the first touch area in the aircraft control interface, acquiring sensor data, and obtaining an aircraft control command according to at least the sensor data, until the touch point Stop when disappearing;
    所述计算机可读指令被所述处理器执行时,还使得所述处理器执行以下步骤:The computer readable instructions, when executed by the processor, further cause the processor to perform the following steps:
    当所述触控点移动到所述飞行器操控界面中的第二触控区域时,根据所述触控点在所述第二触控区域中的位置触发模拟摇杆操控指令并发送到所述飞行器;所述第二触控区域用于模拟摇杆操作。When the touch point moves to the second touch area in the aircraft control interface, triggering an analog joystick manipulation command according to the position of the touch point in the second touch area and transmitting to the The aircraft; the second touch area is used to simulate a joystick operation.
  15. 根据权利要求10所述的移动终端,其特征在于,所述至少根据所述传感器数据得到飞行器操控指令包括:The mobile terminal according to claim 10, wherein the obtaining the aircraft manipulation command based on at least the sensor data comprises:
    根据获取的初始的传感器数据确定传感器所在移动终端的初始状态;Determining an initial state of the mobile terminal where the sensor is located according to the obtained initial sensor data;
    根据获取的初始的传感器数据后续的传感器数据确定所述移动终端的后续状态;及Determining a subsequent state of the mobile terminal according to the acquired sensor data subsequent sensor data; and
    根据所述后续状态相对于所述初始状态的变化生成飞行器操控指令。An aircraft maneuver command is generated based on the change in the subsequent state relative to the initial state.
  16. 根据权利要求10所述的移动终端,其特征在于,所述传感器数据来自于方向传感器、重力传感器、加速度传感器、光线传感器、电子罗盘、距离传感器、三轴陀螺仪传感器、温度传感器以及压力传感器中的至少一种。The mobile terminal according to claim 10, wherein the sensor data is from a direction sensor, a gravity sensor, an acceleration sensor, a light sensor, an electronic compass, a distance sensor, a three-axis gyro sensor, a temperature sensor, and a pressure sensor. At least one of them.
  17. 根据权利要求10所述的移动终端,其特征在于,所述计算机可读指 令被所述处理器执行时,还使得所述处理器执行以下步骤:A mobile terminal according to claim 10, wherein said computer readable finger When executed by the processor, the processor is further caused to perform the following steps:
    检测对所述飞行器操控界面中预设自动操控模式图标的选择指令;Detecting a selection instruction for a preset automatic control mode icon in the aircraft control interface;
    根据所述选择指令确定相应的预设自动操控模式;Determining a corresponding preset automatic control mode according to the selection instruction;
    读取确定的预设自动操控模式所关联的飞行器组合操控指令;及Reading the determined aircraft combination manipulation command associated with the determined preset automatic control mode; and
    向所述飞行器发送所述飞行器组合操控指令,使所述飞行器根据所述飞行器组合操控指令依次执行相应的一系列动作。The aircraft combination steering command is transmitted to the aircraft to cause the aircraft to sequentially perform a corresponding series of actions in accordance with the aircraft combination steering command.
  18. 根据权利要求17所述的移动终端,其特征在于,所述预设自动操控模式包括原地降落模式、返回预设地点降落模式、飞行时紧急悬停模式和跟随锁定目标飞行模式中的至少一种。The mobile terminal according to claim 17, wherein the preset automatic control mode comprises at least one of an in-place landing mode, a return preset landing mode, an in-flight emergency hover mode, and a follow-lock target flight mode. Kind.
  19. 一个或多个存储有计算机可读指令的计算机可读非易失性存储介质,所述计算机可读指令被一个或多个处理器执行时,使得所述一个或多个处理器执行以下步骤:One or more computer readable non-volatile storage media storing computer readable instructions, when executed by one or more processors, cause the one or more processors to perform the steps of:
    显示飞行器操控界面;Display the aircraft control interface;
    检测作用于所述飞行器操控界面的触控操作;Detecting a touch operation acting on the aircraft control interface;
    若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令;及If the touch operation is detected, acquiring sensor data, and obtaining an aircraft manipulation command based on at least the sensor data; and
    向飞行器发送所述飞行器操控指令。The aircraft maneuver command is sent to the aircraft.
  20. 根据权利要求19所述的计算机可读非易失性存储介质,其特征在于,所述若检测到所述触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令包括:The computer readable non-volatile storage medium according to claim 19, wherein if the touch operation is detected, acquiring sensor data and obtaining the aircraft manipulation command based on at least the sensor data comprises:
    若检测到作用于所述飞行器操控界面中第一触控区域的用于开启传感器控制模式的第一触控操作,则获取传感器数据,并至少根据所述传感器数据得到飞行器操控指令,直至检测到作用于所述第一触控区域的第二触控操作时停止。 If the first touch operation for opening the sensor control mode is detected in the first touch area of the aircraft control interface, acquiring sensor data, and obtaining an aircraft control command according to at least the sensor data, until the detection is detected. The second touch operation applied to the first touch area is stopped.
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CN113777996A (en) * 2021-09-23 2021-12-10 东风汽车有限公司东风日产乘用车公司 Remote control method, device and equipment based on mobile terminal

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