WO2018103192A1 - Method and device for maintaining attitude of unmanned aerial vehicle - Google Patents

Method and device for maintaining attitude of unmanned aerial vehicle Download PDF

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Publication number
WO2018103192A1
WO2018103192A1 PCT/CN2017/073112 CN2017073112W WO2018103192A1 WO 2018103192 A1 WO2018103192 A1 WO 2018103192A1 CN 2017073112 W CN2017073112 W CN 2017073112W WO 2018103192 A1 WO2018103192 A1 WO 2018103192A1
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WO
WIPO (PCT)
Prior art keywords
posture
drone
attitude
angle
sensor
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PCT/CN2017/073112
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French (fr)
Chinese (zh)
Inventor
刘均
宋朝忠
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深圳市元征科技股份有限公司
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Publication of WO2018103192A1 publication Critical patent/WO2018103192A1/en

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    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • 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
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

Definitions

  • the present invention relates to the field of UAV control technology, and in particular, to a UAV attitude maintaining method and apparatus.
  • Unmanned aerial vehicles are referred to as "unmanned aerial vehicles” and are unmanned aircraft operated by radio remote control equipment and self-provided program control devices. They are widely used in aerial reconnaissance, surveillance, communication, anti-submarine, electronic interference and other fields.
  • Embodiments of the present invention provide a method and a device for maintaining a posture of a drone, which can monitor the posture of each of the drones and adjust the posture of each position to maintain the posture of the drone more accurately.
  • the present invention provides a UAV attitude maintaining method, including:
  • the location data is at least one of an acceleration and an angular velocity of the preset position of the drone
  • the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle.
  • the method before the calculating the attitude angle according to the location data, the method further includes:
  • the posture of adjusting the preset position of the drone according to the posture angle is specifically:
  • the present invention provides a UAV attitude maintaining device, including:
  • a first acquiring module configured to acquire position data of a preset position of the drone measured by the attitude sensor, where the at least two posture sensors are located at different positions of the drone
  • a calculation module configured to calculate an attitude angle according to the position data
  • an adjustment module configured to adjust a posture of the preset position of the drone according to the posture angle.
  • the location data is at least one of an acceleration and an angular velocity of the preset position of the drone.
  • the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle.
  • the method further includes:
  • a second obtaining module configured to acquire compensation data measured by the compensation sensor, where the compensation sensor is located within the attitude sensor distance threshold;
  • the calculation module is specifically configured to calculate a posture angle according to the position data and the compensation data
  • the method further includes:
  • a receiving module configured to receive a posture adjustment instruction of the user
  • the adjustment module is specifically configured to adjust a posture of the preset position of the UAV according to the posture angle and the posture adjustment instruction.
  • Embodiments of the present invention by acquiring position data of a preset position of a drone measured by an attitude sensor, calculating an attitude angle according to the position data, and adjusting the drone preset according to the posture angle
  • the posture of the position can monitor the posture of each position of the drone and adjust the posture of each position. , to make the drone posture more accurate.
  • FIG. 1 is a flowchart of a method for maintaining a posture of a drone according to an embodiment of the present invention
  • FIG. 2 is a schematic diagram of a specific application scenario
  • FIG. 3 is a flowchart of another UAV attitude maintaining method according to an embodiment of the present invention.
  • FIG. 4 is a schematic structural diagram of a UAV attitude maintaining device according to an embodiment of the present invention.
  • FIG. 5 is a schematic structural diagram of another UAV attitude maintaining device according to an embodiment of the present invention.
  • FIG. 1 is a flowchart of a method for maintaining a posture of a drone according to an embodiment of the present invention, where the method includes the following steps:
  • S101 Acquire location data of a preset position of the drone measured by the attitude sensor, wherein the attitude sensor has at least two, and the attitude sensor is located at different positions of the drone.
  • the attitude sensor is a combined sensor composed of a gyroscope and an acceleration sensor.
  • the gyroscope is a sensing gyroscope, and outputs an angular velocity, and the angle is integrated to obtain an angle. Since the gyroscope still outputs in a zero input state, its output is a white noise and a slowly varying random function. Stack Force, affected by this, in the process of integration, the cumulative error will be introduced, the longer the integral time, the greater the error. Therefore, it is necessary to use an acceleration sensor to correct the gyroscope.
  • the acceleration sensor uses the force decomposition principle to determine the tilt angle by the component of the gravity acceleration in different axial directions. Without the integral error, the error of the gyroscope can be effectively corrected.
  • the attitude sensors are at least two and located at different positions of the drone, and the specific position of the attitude sensor is determined according to the specific situation of the drone.
  • the attitude sensor may be separately mounted on the four axes and the axis of the drone, and the different parts of the four-axis unmanned aerial vehicle Perform posture monitoring.
  • the attitude sensor can be mounted on each side of the drone.
  • the position data is at least one of an acceleration and an angular velocity of the preset position of the UAV, wherein the acceleration is measured by an acceleration sensor in the attitude sensor.
  • the angular velocity is measured by a gyroscope in the attitude sensor.
  • the location data may further include data related to the preset location, such as a height of the preset location from the ground, a distance from the ground control system, and the like.
  • S102 Calculating an attitude angle according to the location data.
  • the attitude angle is calculated by integrating the acceleration sensor and the output of the gyroscope in the attitude sensor, and the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, the pitch The angle, the roll angle, and the yaw angle are respectively formed by the rotation of the preset positions of the drone around the X, ⁇ , and ⁇ axes, and the pitch angle, the roll angle, and the yaw angle reflect the angle The position of the drone's preset position relative to the ground.
  • S103 Adjust a posture of the preset position of the drone according to the posture angle.
  • the drone needs to maintain a posture in various situations. For example, when the drone performs a shooting operation, it is necessary to maintain a certain posture to stabilize the shooting image; In the case of bad weather conditions, the drone needs to maintain a certain posture during flight to improve the anti-interference ability of the drone and prevent the drone from being damaged or unstable.
  • the pitch angle of the preset position of the drone is too large, it indicates that the preset position of the drone is too large relative to the horizontal plane, and may be stabilized by reducing the pitch angle.
  • the preset position If the roll angle of the preset position of the drone is too large, it indicates that the angle of the preset position of the drone is too large, and the posture of the preset position can be stabilized by reducing the roll angle. If the yaw angle of the preset position of the drone is too large, the preset position of the drone is deviated from the route, and the preset position of the drone may be adjusted according to the correct route.
  • different posture sensors are provided at different positions on the drone, and the postures of the different positions are respectively adjusted to maintain the posture of each position of the drone, thereby maintaining the posture of the unmanned body. .
  • a UAV attitude maintaining method obtains a position angle according to a preset position of a UAV measured by an attitude sensor, and calculates an attitude angle according to the position data, according to the The posture angle adjusts the posture of the preset position of the drone, and can effectively monitor the posture of each position of the drone, and adjust the posture of each position, so that the posture of the drone is kept more precise.
  • FIG. 3 is a flowchart of another UAV posture maintaining method according to an embodiment of the present invention, where the method includes the following steps:
  • S301 Acquire location data of a preset position of the drone measured by the attitude sensor, wherein the attitude sensor has at least two, and the attitude sensor is located at different positions of the drone.
  • the attitude sensor is a combined sensor composed of a gyroscope and an acceleration sensor.
  • the gyroscope is a sensing gyroscope, and outputs an angular velocity, and the angle is integrated to obtain an angle. Since the gyroscope still outputs in a zero input state, its output is a white noise and a slowly varying random function. The stacking force is affected by this. In the process of integration, the cumulative error will be introduced. The longer the integral time, the larger the error. Therefore, it is necessary to use an acceleration sensor to correct the gyroscope, and the acceleration sensor is advantageous. Based on the principle of force decomposition, the inclination of the gravitational acceleration in different axial directions is used to judge the inclination. Without the integral error, the error of the gyroscope can be effectively corrected.
  • the attitude sensors are at least two and located at different positions of the drone, and the specific position of the attitude sensor is determined according to the specific situation of the drone.
  • the attitude sensor may be separately mounted on the four axes and the axis of the drone, and the different parts of the four-axis unmanned aerial vehicle Perform posture monitoring.
  • the attitude sensor can be mounted on each side of the drone.
  • the position data is at least one of an acceleration and an angular velocity of the preset position of the drone, wherein the acceleration is measured by an acceleration sensor in the attitude sensor.
  • the angular velocity is measured by a gyroscope in the attitude sensor.
  • the location data may further include data related to the preset location, such as a height of the preset location from the ground, a distance from the ground control system, and the like.
  • S302 Acquire compensation data measured by the compensation sensor, wherein the compensation sensor is located within the attitude sensor distance threshold.
  • S303 Calculate an attitude angle according to the location data and the compensation data.
  • the compensation sensor is located within the attitude sensor distance threshold, and may be configured to equidistantly set a plurality of compensation sensors within the measurement range of the attitude sensor, the composition of the compensation sensor and the The attitude sensor is the same and is used to measure the position data of the position where the compensation sensor is located. Since the flight condition of the UAV is very complicated, the position data provided by the compensation sensor is used as the compensation data of the position data measured by the attitude sensor, and by the compensation filtering process, a more accurate attitude angle can be calculated.
  • the attitude angle is calculated by integrating the output of the attitude sensor and the compensation sensor, and the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, the pitch The angle, the roll angle, and the yaw angle are respectively formed by the rotation of the preset positions of the drone around the X, ⁇ , and ⁇ axes, and the pitch angle, the roll angle, and the yaw angle reflect the angle The position of the drone's preset position relative to the ground.
  • S304 Receive a posture adjustment instruction of the user.
  • the user may issue an attitude adjustment command to the drone through a control terminal, such as a drone remote controller or a ground control system, and the user may according to the actual situation of the flight area of the drone, For example, a weather condition, a number of drones, a geographical situation, etc., to issue an attitude adjustment command to the drone, so that the drone adjusts the flight attitude according to the actual situation of the flight area or the user's demand.
  • a control terminal such as a drone remote controller or a ground control system
  • the drone needs to maintain a posture in various situations. For example, when the drone performs a photographing operation, it is necessary to maintain a certain posture to stabilize the photographing image; In the case of bad weather conditions, the drone needs to maintain a certain posture during flight to improve the anti-interference ability of the drone and prevent the drone from being damaged or unstable.
  • the pitch angle of the preset position of the drone is too large, it indicates that the preset position of the drone is too large relative to the horizontal plane, and may be stabilized by reducing the pitch angle.
  • the attitude of the preset position if the roll angle of the preset position of the drone is too large, it indicates that the angle of the preset position of the drone is too large, and the roll angle can be reduced to stabilize the The posture of the preset position; if the yaw angle of the preset position of the drone is too large, the preset position of the drone is deviated from the route, and the preset position of the drone may be adjusted according to the preset position The correct route travels.
  • the attitude angle indicates a flight attitude of the drone
  • different posture sensors on the unmanned aerial vehicle have different attitude sensors, and respectively adjust postures of different positions to maintain an unmanned position.
  • the posture of each position of the machine, thereby maintaining the posture of the unmanned body, and the unmanned aerial vehicle adjusting the posture according to the posture adjustment command sent by the user can adapt the drone to the flight environment and the user's demand, Adjusting the man-machine according to the posture angle and the posture adjustment command can better maintain the posture of the preset position of the drone.
  • a UAV attitude maintaining method acquires compensation data measured by a compensation sensor by acquiring position data of a preset position of the UAV measured by the attitude sensor, according to the position data and The compensation data calculates an attitude angle, receives a posture adjustment instruction of the user, adjusts a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction, and can effectively monitor each position of the drone Attitude situation, and posture adjustment of each position to maintain the attitude of the drone More precise.
  • FIG. 4 is a schematic structural diagram of a UAV attitude maintaining device according to an embodiment of the present invention.
  • the device is applied to a UAV, and the device 400 includes the following functional modules:
  • the first obtaining module 410 is configured to acquire location data of a preset position of the drone measured by the attitude sensor
  • the attitude sensor has at least two, and the attitude sensor is located at different positions of the drone.
  • the attitude sensor is a combined sensor composed of a gyroscope and an acceleration sensor.
  • the gyroscope is a sensing gyroscope, and outputs an angular velocity, and the angle is integrated to obtain an angle. Since the gyroscope still outputs in a zero input state, its output is a white noise and a slowly varying random function. The stacking force is affected by this. In the process of integration, the cumulative error will be introduced. The longer the integral time, the larger the error. Therefore, it is necessary to use an acceleration sensor to correct the gyroscope.
  • the acceleration sensor uses the force decomposition principle to determine the tilt angle by the component of the gravity acceleration in different axial directions. Without the integral error, the error of the gyroscope can be effectively corrected.
  • the attitude sensors are at least two and located at different positions of the drone, and the specific position of the attitude sensor is determined according to the specific situation of the drone.
  • the attitude sensor may be separately mounted on the four axes and the axis of the drone, and the different parts of the four-axis unmanned aerial vehicle Perform posture monitoring.
  • the attitude sensor can be mounted on each side of the drone.
  • the position data is at least one of an acceleration and an angular velocity of the preset position of the drone, wherein the acceleration is measured by an acceleration sensor in the attitude sensor, The angular velocity is measured by a gyroscope in the attitude sensor.
  • the location data may further include data related to the preset location, such as a height of the preset location from the ground, a distance from the ground control system, and the like.
  • the calculation module 420 is configured to calculate an attitude angle according to the location data.
  • the output of the acceleration sensor and the gyroscope in the attitude sensor is integrated to calculate Obtaining an attitude angle, wherein the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, wherein the pitch angle, the roll angle, and the yaw angle are respectively preset positions of the drone around X, ⁇ ,
  • the angle formed by the rotation of the three axes respectively, the pitch angle, the roll angle, and the yaw angle reflect the posture of the preset position of the drone relative to the ground.
  • the adjustment module 430 is configured to adjust a posture of the preset position of the drone according to the posture angle.
  • the drone needs to maintain a posture in various situations. For example, when the drone performs a shooting operation, it is necessary to maintain a certain posture to stabilize the shooting image; In the case of bad weather conditions, the drone needs to maintain a certain posture during flight to improve the anti-interference ability of the drone and prevent the drone from being damaged or unstable.
  • the pitch angle of the preset position of the drone is too large, it indicates that the preset position of the drone is too large relative to the horizontal plane, and may be stabilized by reducing the pitch angle.
  • the attitude of the preset position if the roll angle of the preset position of the drone is too large, it indicates that the angle of the preset position of the drone is too large, and the roll angle can be reduced to stabilize the The posture of the preset position; if the yaw angle of the preset position of the drone is too large, the preset position of the drone is deviated from the route, and the preset position of the drone may be adjusted according to the preset position The correct route travels.
  • different posture sensors are provided at different positions on the drone, and the postures of the different positions are respectively adjusted to maintain the posture of each position of the drone, thereby maintaining the posture of the unmanned body. .
  • a UAV attitude maintaining device 400 can implement the UAV attitude maintaining method as shown in FIG. 1. For details, refer to FIG. 1 and related embodiments, and details are not described herein again.
  • a UAV attitude maintaining device obtains a position angle according to a preset position of a UAV measured by an attitude sensor, and calculates an attitude angle according to the position data, according to the The posture angle adjusts the posture of the preset position of the drone, and can effectively monitor the posture of each position of the drone, and adjust the posture of each position, so that the posture of the drone is kept more precise.
  • FIG. 5 is another UAV attitude maintaining device according to an embodiment of the present invention.
  • the device is applied to a UAV, and the difference between the device 500 and the device 400 shown in FIG. It also includes the following functional modules:
  • a second obtaining module 440 configured to acquire compensation data measured by the compensation sensor, where the compensation transmission The sensor is located within the attitude sensor distance threshold;
  • the calculation module is specifically configured to calculate a posture angle according to the position data and the compensation data
  • the compensation sensor is located within the attitude sensor distance threshold, and may be configured to equidistantly set a plurality of compensation sensors within the measurement range of the attitude sensor, the composition of the compensation sensor and the The attitude sensor is the same and is used to measure the position data of the position where the compensation sensor is located. Since the flight condition of the UAV is very complicated, the position data provided by the compensation sensor is used as the compensation data of the position data measured by the attitude sensor, and by the compensation filtering process, a more accurate attitude angle can be calculated.
  • the attitude angle is calculated by integrating the output of the attitude sensor and the compensation sensor, and the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, the pitch The angle, the roll angle, and the yaw angle are respectively formed by the rotation of the preset positions of the drone around the X, ⁇ , and ⁇ axes, and the pitch angle, the roll angle, and the yaw angle reflect the angle The position of the drone's preset position relative to the ground.
  • the receiving module 450 is configured to receive a posture adjustment instruction of the user
  • the adjustment module is specifically configured to adjust a posture of the preset position of the UAV according to the posture angle and the posture adjustment instruction.
  • the user may issue an attitude adjustment command to the drone through a control terminal, such as a drone remote controller or a ground control system, and the user may according to the actual situation of the flight area of the drone, For example, a weather condition, a number of drones, a geographical situation, etc., to issue an attitude adjustment command to the drone, so that the drone adjusts the flight attitude according to the actual situation of the flight area or the user's demand.
  • a control terminal such as a drone remote controller or a ground control system
  • the attitude angle indicates a flight attitude of the drone
  • different posture sensors on the unmanned aerial vehicle have different attitude sensors, and respectively adjust attitudes of different positions to maintain an unmanned position.
  • the posture of each position of the machine, thereby maintaining the posture of the unmanned body, and the unmanned aerial vehicle adjusting the posture according to the posture adjustment command sent by the user can adapt the drone to the flight environment and the user's demand, Adjusting the man-machine according to the posture angle and the posture adjustment command can better maintain the posture of the preset position of the drone.
  • the UAV posture maintaining device 500 of the embodiment of the present invention can implement the UAV attitude maintaining method as shown in FIG. 3, and specifically refer to FIG. 3 and related embodiments, where Repeat
  • a UAV attitude maintaining device acquires compensation data measured by a compensation sensor by acquiring position data of a preset position of the UAV measured by the attitude sensor, according to the position data and The compensation data calculates an attitude angle, receives a posture adjustment instruction of the user, adjusts a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction, and can effectively monitor each position of the drone Attitude situation, and posture adjustment of each position, so that the attitude of the drone is kept more precise.
  • the storage medium may be a magnetic disk, an optical disk, or a read-only storage memory (Read-Only)
  • ROM Read Only Memory
  • RAM Random Access Memory

Abstract

A method and device for maintaining an attitude of an unmanned aerial vehicle. The method for maintaining an attitude of an unmanned aerial vehicle comprises: obtaining position data of a preset position of an unmanned aerial vehicle measured by attitude sensors, there being at least two attitude sensors located at different positions on the unmanned aerial vehicle (S101); calculating an attitude angle according to the position data (S102); and adjusting the attitude of the unmanned aerial vehicle at the preset position according to the attitude angle (S103). The method for maintaining an attitude of an unmanned aerial vehicle can monitor attitudes of an unmanned aerial vehicle at different positions in real time and adjust the attitudes at different positions, thereby more precisely maintaining the attitudes of the unmanned aerial vehicle.

Description

一种无人机姿态保持方法及装置  Unmanned aerial vehicle attitude maintaining method and device
[0001] 技术领域  [0001] Technical Field
[0002] 本发明涉及无人机控制技术领域, 特别涉及一种无人机姿态保持方法及装置。  [0002] The present invention relates to the field of UAV control technology, and in particular, to a UAV attitude maintaining method and apparatus.
[0003] 背景技术 BACKGROUND
[0004] 无人驾驶飞机简称"无人机", 是利用无线电遥控设备和自备的程序控制装置操 纵的不载人飞机, 广泛应用于空中侦察、 监视、 通信、 反潜、 电子干扰等领域  [0004] Unmanned aerial vehicles are referred to as "unmanned aerial vehicles" and are unmanned aircraft operated by radio remote control equipment and self-provided program control devices. They are widely used in aerial reconnaissance, surveillance, communication, anti-submarine, electronic interference and other fields.
[0005] 目前, 现有的无人机在空中作业吋, 常常需要在一段吋间内保持一定的姿态, 以便于更好地工作, 现有技术中主要是通过在无人机体的几何中心安装一个陀 螺仪和加速度计组成的传感系统来获取无人机飞行吋的姿态数据, 然后根据所 述姿态数据通过遥控或者自我调节实现无人机的姿态保持。 但无人机在空中作 业吋情况复杂多变, 根据所述姿态数据不能精确地保持无人机的姿态。 [0005] At present, existing drones operate in the air, often need to maintain a certain posture in a period of time to facilitate better work, the prior art is mainly installed in the geometric center of the unmanned body. A sensing system consisting of a gyroscope and an accelerometer acquires the attitude data of the drone's flying raft, and then maintains the attitude of the drone by remote control or self-adjustment according to the posture data. However, the situation of the drone in the air is complicated and varied, and the posture of the drone cannot be accurately maintained according to the posture data.
[0006] 发明内容  SUMMARY OF THE INVENTION
[0007] 本发明实施例提供一种无人机姿态保持方法及装置, 能够随吋监控无人机各位 置的姿态情况, 并进行各位置的姿态调整, 使无人机姿态保持更精准。  [0007] Embodiments of the present invention provide a method and a device for maintaining a posture of a drone, which can monitor the posture of each of the drones and adjust the posture of each position to maintain the posture of the drone more accurately.
[0008] 第一方面, 本发明提供了一种无人机姿态保持方法, 包括:  [0008] In a first aspect, the present invention provides a UAV attitude maintaining method, including:
[0009] 获取姿态传感器测量的无人机的预设位置的位置数据, 其中, 所述姿态传感器 至少有两个, 所述姿态传感器位于所述无人机的不同位置;  [0009] acquiring position data of a preset position of the drone measured by the attitude sensor, wherein the attitude sensor has at least two, and the attitude sensor is located at different positions of the drone;
[0010] 根据所述位置数据计算得出姿态角;  [0010] calculating an attitude angle according to the position data;
[0011] 根据所述姿态角调整所述无人机预设位置的姿态。  [0011] adjusting a posture of the preset position of the drone according to the posture angle.
[0012] 优选地, 所述位置数据为所述无人机预设位置的加速度、 角速度中的至少一个  [0012] Preferably, the location data is at least one of an acceleration and an angular velocity of the preset position of the drone
[0013] 优选地, 所述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个。 [0013] Preferably, the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle.
[0014] 优选地, 在所述根据所述位置数据计算得出姿态角之前, 还包括: [0014] Preferably, before the calculating the attitude angle according to the location data, the method further includes:
[0015] 获取补偿传感器测量的补偿数据, 其中, 所述补偿传感器位于所述姿态传感器 距离阈值内; [0016] 所述根据所述位置数据计算得出姿态角具体为: [0015] acquiring compensation data measured by the compensation sensor, wherein the compensation sensor is located within the attitude sensor distance threshold; [0016] The calculated attitude angle according to the location data is specifically:
[0017] 根据所述位置数据以及所述补偿数据计算得出姿态角。  [0017] calculating an attitude angle based on the position data and the compensation data.
[0018] 优选地, 在所述根据所述姿态角调整所述无人机预设位置的姿态之前, 还包括  [0018] Preferably, before the adjusting the posture of the preset position of the drone according to the posture angle,
[0019] 接收用户的姿态调整指令; Receiving a posture adjustment instruction of the user;
[0020] 所述根据所述姿态角调整所述无人机预设位置的姿态具体为:  [0020] the posture of adjusting the preset position of the drone according to the posture angle is specifically:
[0021] 根据所述姿态角以及所述姿态调整指令调整所述无人机预设位置的姿态。  And [0021] adjusting a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction.
[0022] 第二方面, 本发明提供了一种无人机姿态保持装置, 包括:  [0022] In a second aspect, the present invention provides a UAV attitude maintaining device, including:
[0023] 第一获取模块, 用于获取姿态传感器测量的无人机的预设位置的位置数据, 其 中, 所述姿态传感器至少有两个, 所述姿态传感器位于所述无人机的不同位置  [0023] a first acquiring module, configured to acquire position data of a preset position of the drone measured by the attitude sensor, where the at least two posture sensors are located at different positions of the drone
[0024] 计算模块, 用于根据所述位置数据计算得出姿态角; [0024] a calculation module, configured to calculate an attitude angle according to the position data;
[0025] 调整模块, 用于根据所述姿态角调整所述无人机预设位置的姿态。  [0025] an adjustment module, configured to adjust a posture of the preset position of the drone according to the posture angle.
[0026] 优选地, 所述位置数据为所述无人机预设位置的加速度、 角速度中的至少一个  [0026] Preferably, the location data is at least one of an acceleration and an angular velocity of the preset position of the drone.
[0027] 优选地, 所述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个。 [0027] Preferably, the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle.
[0028] 优选地, 还包括: [0028] Preferably, the method further includes:
[0029] 第二获取模块, 用于获取补偿传感器测量的补偿数据, 其中, 所述补偿传感器 位于所述姿态传感器距离阈值内;  [0029] a second obtaining module, configured to acquire compensation data measured by the compensation sensor, where the compensation sensor is located within the attitude sensor distance threshold;
[0030] 所述计算模块具体用于, 根据所述位置数据以及所述补偿数据计算得出姿态角 [0030] the calculation module is specifically configured to calculate a posture angle according to the position data and the compensation data
[0031] 优选地, 还包括: [0031] Preferably, the method further includes:
[0032] 接收模块, 用于接收用户的姿态调整指令;  [0032] a receiving module, configured to receive a posture adjustment instruction of the user;
[0033] 所述调整模块具体用于, 根据所述姿态角以及所述姿态调整指令调整所述无人 机预设位置的姿态。  [0033] The adjustment module is specifically configured to adjust a posture of the preset position of the UAV according to the posture angle and the posture adjustment instruction.
[0034] 实施本发明实施例, 通过获取姿态传感器测量的无人机的预设位置的位置数据 , 根据所述位置数据计算得出姿态角, 根据所述姿态角调整所述无人机预设位 置的姿态, 能够实吋监控无人机各位置的姿态情况, 并进行各位置的姿态调整 , 使无人机姿态保持更精准。 [0034] Embodiments of the present invention, by acquiring position data of a preset position of a drone measured by an attitude sensor, calculating an attitude angle according to the position data, and adjusting the drone preset according to the posture angle The posture of the position can monitor the posture of each position of the drone and adjust the posture of each position. , to make the drone posture more accurate.
[0035] 附图说明  BRIEF DESCRIPTION OF THE DRAWINGS
[0036] 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。  [0036] 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 prior art description will be briefly described below, and obviously, in the following description The drawings 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.
[0037] 图 1是本发明实施例提供的一种无人机姿态保持方法的流程图;  1 is a flowchart of a method for maintaining a posture of a drone according to an embodiment of the present invention;
[0038] 图 2是一具体应用场景的示意图;  2 is a schematic diagram of a specific application scenario;
[0039] 图 3是本发明实施例提供的另一种无人机姿态保持方法的流程图;  3 is a flowchart of another UAV attitude maintaining method according to an embodiment of the present invention;
[0040] 图 4是本发明实施例提供的一种无人机姿态保持装置的结构示意图; 4 is a schematic structural diagram of a UAV attitude maintaining device according to an embodiment of the present invention;
[0041] 图 5是本发明实施例提供的另一种无人机姿态保持装置的结构示意图。 FIG. 5 is a schematic structural diagram of another UAV attitude maintaining device according to an embodiment of the present invention.
[0042] 具体实施方式 DETAILED DESCRIPTION
[0043] 下面将结合本发明实施例中的附图, 对本发明实施例中的技术方案进行清楚、 完整地描述, 显然, 所描述的实施例仅仅是本发明一部分实施例, 而不是全部 的实施例。 基于本发明中的实施例, 本领域普通技术人员在没有作出创造性劳 动前提下所获得的所有其他实施例, 都属于本发明保护的范围。  The technical solutions in the embodiments of the present invention are clearly and completely described in the following with reference to the accompanying drawings in the embodiments of the present invention. It is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. example. All other embodiments obtained by a person of ordinary skill in the art based on the embodiments of the present invention without creative efforts are within the scope of the present invention.
[0044] 需要说明的是, 在本发明实施例中使用的术语是仅仅出于描述特定实施例的目 的, 而非旨在限制本发明。 在本发明实施例和所附权利要求书中所使用的单数 形式的 "一种"、 "所述 "和"该"也旨在包括多数形式, 除非上下文清楚地表示其他 含义。 还应当理解, 本文中使用的术语"和 /或"是指并包含一个或多个相关联的 列出项目的任何或所有可能组合。  [0044] It is to be understood that the terminology used in the embodiments of the present invention is for the purpose of describing particular embodiments, and is not intended to limit the invention. The singular forms "a", "the" and "the" It should also be understood that the term "and/or" as used herein refers to and encompasses any and all possible combinations of one or more of the associated listed items.
[0045] 请参阅图 1, 图 1是本发明实施例提供的一种无人机姿态保持方法的流程图, 所 述方法包括以下步骤:  Referring to FIG. 1, FIG. 1 is a flowchart of a method for maintaining a posture of a drone according to an embodiment of the present invention, where the method includes the following steps:
[0046] S101 : 获取姿态传感器测量的无人机的预设位置的位置数据, 其中, 所述姿态 传感器至少有两个, 所述姿态传感器位于所述无人机的不同位置。  [0046] S101: Acquire location data of a preset position of the drone measured by the attitude sensor, wherein the attitude sensor has at least two, and the attitude sensor is located at different positions of the drone.
[0047] 所述姿态传感器为组合式传感器, 由陀螺仪和加速度传感器组成。 其中, 所述 陀螺仪为传感陀螺仪, 输出角速度, 对所述角速度进行积分能得到角度, 由于 所述陀螺仪在零输入状态吋仍有输出, 它的输出是白噪声和慢变随机函数的叠 力口, 受此影响, 在积分的过程中, 会引进累计误差, 积分吋间越长, 误差就越 大。 因此, 需要利用加速度传感器来对陀螺仪进行校正, 所述加速度传感器利 用力的分解原理, 通过重力加速度在不同轴向上的分量来判断倾角, 没有积分 误差, 可以有效校正陀螺仪的误差。 [0047] The attitude sensor is a combined sensor composed of a gyroscope and an acceleration sensor. Wherein, the gyroscope is a sensing gyroscope, and outputs an angular velocity, and the angle is integrated to obtain an angle. Since the gyroscope still outputs in a zero input state, its output is a white noise and a slowly varying random function. Stack Force, affected by this, in the process of integration, the cumulative error will be introduced, the longer the integral time, the greater the error. Therefore, it is necessary to use an acceleration sensor to correct the gyroscope. The acceleration sensor uses the force decomposition principle to determine the tilt angle by the component of the gravity acceleration in different axial directions. Without the integral error, the error of the gyroscope can be effectively corrected.
[0048] 所述姿态传感器至少有两个, 且位于所述无人机的不同位置, 所述姿态传感器 的具体位置根据所述无人机的具体情况确定。 在一具体的实施例中, 若无人机 为四轴无人飞行器, 那么可以在所述无人机的四轴以及轴心上分别安装所述姿 态传感器, 对四轴无人飞行器不同的部位进行姿态监控。 在另一实施例中, 若 无人机为双翼无人飞机, 那么可以在所述无人机两边的侧翼上分别安装所述姿 态传感器。  [0048] The attitude sensors are at least two and located at different positions of the drone, and the specific position of the attitude sensor is determined according to the specific situation of the drone. In a specific embodiment, if the drone is a four-axis unmanned aerial vehicle, the attitude sensor may be separately mounted on the four axes and the axis of the drone, and the different parts of the four-axis unmanned aerial vehicle Perform posture monitoring. In another embodiment, if the drone is a two-wing unmanned aircraft, the attitude sensor can be mounted on each side of the drone.
[0049] 在本实施方式中, 所述位置数据为所述无人机预设位置的加速度、 角速度中的 至少一个, 其中, 所述加速度由所述姿态传感器中的加速度传感器测量得出, 所述角速度由所述姿态传感器中的陀螺仪测量得出。 在其他实施方式中, 所述 位置数据还可以包括所述预设位置距离地面的高度、 和地面控制系统的距离等 与所述预设位置相关的数据。  [0049] In the embodiment, the position data is at least one of an acceleration and an angular velocity of the preset position of the UAV, wherein the acceleration is measured by an acceleration sensor in the attitude sensor. The angular velocity is measured by a gyroscope in the attitude sensor. In other embodiments, the location data may further include data related to the preset location, such as a height of the preset location from the ground, a distance from the ground control system, and the like.
[0050] S102: 根据所述位置数据计算得出姿态角。  [0050] S102: Calculating an attitude angle according to the location data.
[0051] 在本实施方式中, 综合姿态传感器中的加速度传感器和陀螺仪的输出, 来计算 得出姿态角, 述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个, 所述俯仰 角、 滚转角、 偏航角分别是所述无人机的预设位置围绕 X、 Υ、 Ζ三个轴分别转 动形成的夹角, 所述俯仰角、 滚转角、 偏航角反映了所述无人机预设位置相对 地面的姿态。  [0051] In the present embodiment, the attitude angle is calculated by integrating the acceleration sensor and the output of the gyroscope in the attitude sensor, and the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, the pitch The angle, the roll angle, and the yaw angle are respectively formed by the rotation of the preset positions of the drone around the X, Υ, and 轴 axes, and the pitch angle, the roll angle, and the yaw angle reflect the angle The position of the drone's preset position relative to the ground.
[0052] S103: 根据所述姿态角调整所述无人机预设位置的姿态。  [0052] S103: Adjust a posture of the preset position of the drone according to the posture angle.
[0053] 在本实施方式中, 所述无人机在多种情况下都需要保持姿态, 例如, 当所述无 人机进行拍摄作业吋, 需要保持一定的姿态以使拍摄画面稳定; 当所述无人机 在天气状况恶劣的情况下, 在飞行吋需要保持一定的姿态以提高无人机的抗干 扰能力, 防止无人机损坏或失稳。  [0053] In the embodiment, the drone needs to maintain a posture in various situations. For example, when the drone performs a shooting operation, it is necessary to maintain a certain posture to stabilize the shooting image; In the case of bad weather conditions, the drone needs to maintain a certain posture during flight to improve the anti-interference ability of the drone and prevent the drone from being damaged or unstable.
[0054] 具体的, 若所述无人机预设位置的俯仰角过大, 则说明所述无人机预设位置相 对于水平面上下的幅度过大, 可以通过减小所述俯仰角来稳定所述预设位置的 姿态; 若所述无人机预设位置的滚转角过大, 则说明所述无人机预设位置翻转 的角度过大, 可以通过减小所述滚转角来稳定所述预设位置的姿态; 若所述无 人机预设位置的偏航角过大, 则说明所述无人机预设位置偏离了航线, 可以通 过调整使所述无人机预设位置按照正确的航线行进。 [0054] Specifically, if the pitch angle of the preset position of the drone is too large, it indicates that the preset position of the drone is too large relative to the horizontal plane, and may be stabilized by reducing the pitch angle. The preset position If the roll angle of the preset position of the drone is too large, it indicates that the angle of the preset position of the drone is too large, and the posture of the preset position can be stabilized by reducing the roll angle. If the yaw angle of the preset position of the drone is too large, the preset position of the drone is deviated from the route, and the preset position of the drone may be adjusted according to the correct route.
[0055] 在本实施方式中, 所述无人机上不同的位置有不同的姿态传感器, 分别对不同 位置的姿态进行调整, 能够保持无人机每个位置的姿态, 进而保持无人机体的 姿态。  [0055] In the embodiment, different posture sensors are provided at different positions on the drone, and the postures of the different positions are respectively adjusted to maintain the posture of each position of the drone, thereby maintaining the posture of the unmanned body. .
[0056] 为了便于对本发明实施例进行理解, 下面结合具体的应用场景进行说明。  [0056] In order to facilitate the understanding of the embodiments of the present invention, the following describes the specific application scenarios.
[0057] 无人机在进行拍摄工作吋, 需要进行姿态保持以保证拍摄画面清晰稳定, 但在 拍摄过程中突然遇到向下的大风, 导致无人机机头向下偏离, 导致拍摄画面不 稳定, 而且有可能导致无人机飞行失控而损坏。 假设所述无人机在机头位置安 装有姿态传感器, 那么在所述无人机飞行过程中, 所述姿态传感器能够实吋测 量所述无人机机头的位置数据, 在所述无人机机头发生偏离吋, 能够计算得出 所述无人机机头的俯仰角, 所述无人机能够根据所述俯仰角自行调节机头的姿 态, 保持飞行姿态。 参阅图 2, 图 2为具体应用场景的示意图。  [0057] When the drone is performing the shooting work, it is necessary to maintain the posture to ensure that the shooting picture is clear and stable, but suddenly encounters a downward wind during the shooting process, causing the drone head to deviate downward, resulting in no shooting picture. Stable, and may cause the drone to fly out of control and damage. Assuming that the drone is equipped with an attitude sensor at the head position, the attitude sensor can measure the position data of the drone head during the flight of the drone, When the nose of the machine head is deviated, the pitch angle of the nose of the drone can be calculated, and the drone can adjust the attitude of the nose according to the pitch angle to maintain the flight attitude. Refer to Figure 2, which is a schematic diagram of a specific application scenario.
[0058] 上述可知, 本发明实施例的一种无人机姿态保持方法通过获取姿态传感器测量 的无人机的预设位置的位置数据, 根据所述位置数据计算得出姿态角, 根据所 述姿态角调整所述无人机预设位置的姿态, 能够实吋监控无人机各位置的姿态 情况, 并进行各位置的姿态调整, 使无人机姿态保持更精准。  [0058] As described above, a UAV attitude maintaining method according to an embodiment of the present invention obtains a position angle according to a preset position of a UAV measured by an attitude sensor, and calculates an attitude angle according to the position data, according to the The posture angle adjusts the posture of the preset position of the drone, and can effectively monitor the posture of each position of the drone, and adjust the posture of each position, so that the posture of the drone is kept more precise.
[0059] 请参阅图 3, 图 3是本发明实施例提供的另一种无人机姿态保持方法的流程图, 所述方法包括以下步骤:  Referring to FIG. 3, FIG. 3 is a flowchart of another UAV posture maintaining method according to an embodiment of the present invention, where the method includes the following steps:
[0060] S301 : 获取姿态传感器测量的无人机的预设位置的位置数据, 其中, 所述姿态 传感器至少有两个, 所述姿态传感器位于所述无人机的不同位置。  [0060] S301: Acquire location data of a preset position of the drone measured by the attitude sensor, wherein the attitude sensor has at least two, and the attitude sensor is located at different positions of the drone.
[0061] 所述姿态传感器为组合式传感器, 由陀螺仪和加速度传感器组成。 其中, 所述 陀螺仪为传感陀螺仪, 输出角速度, 对所述角速度进行积分能得到角度, 由于 所述陀螺仪在零输入状态吋仍有输出, 它的输出是白噪声和慢变随机函数的叠 力口, 受此影响, 在积分的过程中, 会引进累计误差, 积分吋间越长, 误差就越 大。 因此, 需要利用加速度传感器来对陀螺仪进行校正, 所述加速度传感器利 用力的分解原理, 通过重力加速度在不同轴向上的分量来判断倾角, 没有积分 误差, 可以有效校正陀螺仪的误差。 [0061] The attitude sensor is a combined sensor composed of a gyroscope and an acceleration sensor. Wherein, the gyroscope is a sensing gyroscope, and outputs an angular velocity, and the angle is integrated to obtain an angle. Since the gyroscope still outputs in a zero input state, its output is a white noise and a slowly varying random function. The stacking force is affected by this. In the process of integration, the cumulative error will be introduced. The longer the integral time, the larger the error. Therefore, it is necessary to use an acceleration sensor to correct the gyroscope, and the acceleration sensor is advantageous. Based on the principle of force decomposition, the inclination of the gravitational acceleration in different axial directions is used to judge the inclination. Without the integral error, the error of the gyroscope can be effectively corrected.
[0062] 所述姿态传感器至少有两个, 且位于所述无人机的不同位置, 所述姿态传感器 的具体位置根据所述无人机的具体情况确定。 在一具体的实施例中, 若无人机 为四轴无人飞行器, 那么可以在所述无人机的四轴以及轴心上分别安装所述姿 态传感器, 对四轴无人飞行器不同的部位进行姿态监控。 在另一实施例中, 若 无人机为双翼无人飞机, 那么可以在所述无人机两边的侧翼上分别安装所述姿 态传感器。  [0062] The attitude sensors are at least two and located at different positions of the drone, and the specific position of the attitude sensor is determined according to the specific situation of the drone. In a specific embodiment, if the drone is a four-axis unmanned aerial vehicle, the attitude sensor may be separately mounted on the four axes and the axis of the drone, and the different parts of the four-axis unmanned aerial vehicle Perform posture monitoring. In another embodiment, if the drone is a two-wing unmanned aircraft, the attitude sensor can be mounted on each side of the drone.
[0063] 在本实施方式中, 所述位置数据为所述无人机预设位置的加速度、 角速度中的 至少一个, 其中, 所述加速度由所述姿态传感器中的加速度传感器测量得出, 所述角速度由所述姿态传感器中的陀螺仪测量得出。 在其他实施方式中, 所述 位置数据还可以包括所述预设位置距离地面的高度、 和地面控制系统的距离等 与所述预设位置相关的数据。  [0063] In the embodiment, the position data is at least one of an acceleration and an angular velocity of the preset position of the drone, wherein the acceleration is measured by an acceleration sensor in the attitude sensor. The angular velocity is measured by a gyroscope in the attitude sensor. In other embodiments, the location data may further include data related to the preset location, such as a height of the preset location from the ground, a distance from the ground control system, and the like.
[0064] S302: 获取补偿传感器测量的补偿数据, 其中, 所述补偿传感器位于所述姿态 传感器距离阈值内。  [0064] S302: Acquire compensation data measured by the compensation sensor, wherein the compensation sensor is located within the attitude sensor distance threshold.
[0065] S303: 根据所述位置数据以及所述补偿数据计算得出姿态角。  [0065] S303: Calculate an attitude angle according to the location data and the compensation data.
[0066] 在本实施方式中, 所述补偿传感器位于所述姿态传感器距离阈值内, 可以是在 所述姿态传感器的测量范围内等距离设置多个补偿传感器, 所述补偿传感器的 组成和所述姿态传感器相同, 用于测量所述补偿传感器所处位置的位置数据。 由于无人机飞行吋情况十分复杂, 所述补偿传感器提供的位置数据作为所述姿 态传感器测量出的位置数据的补偿数据, 通过补偿滤波处理, 能够计算得出更 加准确的姿态角。  [0066] In the embodiment, the compensation sensor is located within the attitude sensor distance threshold, and may be configured to equidistantly set a plurality of compensation sensors within the measurement range of the attitude sensor, the composition of the compensation sensor and the The attitude sensor is the same and is used to measure the position data of the position where the compensation sensor is located. Since the flight condition of the UAV is very complicated, the position data provided by the compensation sensor is used as the compensation data of the position data measured by the attitude sensor, and by the compensation filtering process, a more accurate attitude angle can be calculated.
[0067] 在本实施方式中, 综合所述姿态传感器和所述补偿传感器的输出, 来计算得出 姿态角, 述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个, 所述俯仰角、 滚转角、 偏航角分别是所述无人机的预设位置围绕 X、 Υ、 Ζ三个轴分别转动形 成的夹角, 所述俯仰角、 滚转角、 偏航角反映了所述无人机预设位置相对地面 的姿态。  [0067] In the present embodiment, the attitude angle is calculated by integrating the output of the attitude sensor and the compensation sensor, and the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, the pitch The angle, the roll angle, and the yaw angle are respectively formed by the rotation of the preset positions of the drone around the X, Υ, and 轴 axes, and the pitch angle, the roll angle, and the yaw angle reflect the angle The position of the drone's preset position relative to the ground.
[0068] S304: 接收用户的姿态调整指令。 [0069] 在本实施方式中, 用户可以通过控制终端, 例如无人机遥控器或者地面控制系 统对无人机发出姿态调整指令, 所述用户可以根据所述无人机飞行区域的实际 情况、 例如天气状况、 无人机数量、 地理情况等来对所述无人机发出姿态调整 指令, 以使所述无人机根据飞行区域的实际情况或者用户需求来调整飞行姿态 [0068] S304: Receive a posture adjustment instruction of the user. [0069] In this embodiment, the user may issue an attitude adjustment command to the drone through a control terminal, such as a drone remote controller or a ground control system, and the user may according to the actual situation of the flight area of the drone, For example, a weather condition, a number of drones, a geographical situation, etc., to issue an attitude adjustment command to the drone, so that the drone adjusts the flight attitude according to the actual situation of the flight area or the user's demand.
[0070] S305: 根据所述姿态角以及所述姿态调整指令调整所述无人机预设位置的姿态 [0070] S305: Adjust a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction
[0071] 在本实施方式中, 所述无人机在多种情况下都需要保持姿态, 例如, 当所述无 人机进行拍摄作业吋, 需要保持一定的姿态以使拍摄画面稳定; 当所述无人机 在天气状况恶劣的情况下, 在飞行吋需要保持一定的姿态以提高无人机的抗干 扰能力, 防止无人机损坏或失稳。 [0071] In the embodiment, the drone needs to maintain a posture in various situations. For example, when the drone performs a photographing operation, it is necessary to maintain a certain posture to stabilize the photographing image; In the case of bad weather conditions, the drone needs to maintain a certain posture during flight to improve the anti-interference ability of the drone and prevent the drone from being damaged or unstable.
[0072] 具体的, 若所述无人机预设位置的俯仰角过大, 则说明所述无人机预设位置相 对于水平面上下的幅度过大, 可以通过减小所述俯仰角来稳定所述预设位置的 姿态; 若所述无人机预设位置的滚转角过大, 则说明所述无人机预设位置翻转 的角度过大, 可以通过减小所述滚转角来稳定所述预设位置的姿态; 若所述无 人机预设位置的偏航角过大, 则说明所述无人机预设位置偏离了航线, 可以通 过调整使所述无人机预设位置按照正确的航线行进。  [0072] Specifically, if the pitch angle of the preset position of the drone is too large, it indicates that the preset position of the drone is too large relative to the horizontal plane, and may be stabilized by reducing the pitch angle. The attitude of the preset position; if the roll angle of the preset position of the drone is too large, it indicates that the angle of the preset position of the drone is too large, and the roll angle can be reduced to stabilize the The posture of the preset position; if the yaw angle of the preset position of the drone is too large, the preset position of the drone is deviated from the route, and the preset position of the drone may be adjusted according to the preset position The correct route travels.
[0073] 在本实施方式中, 所述姿态角表明所述无人机的飞行姿态, 所述无人机上不同 的位置有不同的姿态传感器, 分别对不同位置的姿态进行调整, 能够保持无人 机每个位置的姿态, 进而保持无人机体的姿态, 同吋, 所述无人机根据用户发 送的姿态调整指令来调整姿态能够使所述无人机适应飞行环境和用户需求, 所 述无人机根据所述姿态角以及所述姿态调整指令进行调整能够更好地保持所述 无人机预设位置的姿态。  [0073] In the embodiment, the attitude angle indicates a flight attitude of the drone, and different posture sensors on the unmanned aerial vehicle have different attitude sensors, and respectively adjust postures of different positions to maintain an unmanned position. The posture of each position of the machine, thereby maintaining the posture of the unmanned body, and the unmanned aerial vehicle adjusting the posture according to the posture adjustment command sent by the user can adapt the drone to the flight environment and the user's demand, Adjusting the man-machine according to the posture angle and the posture adjustment command can better maintain the posture of the preset position of the drone.
[0074] 上述可知, 本发明实施例的一种无人机姿态保持方法通过获取姿态传感器测量 的无人机的预设位置的位置数据, 获取补偿传感器测量的补偿数据, 根据所述 位置数据以及所述补偿数据计算得出姿态角, 接收用户的姿态调整指令, 根据 所述姿态角以及所述姿态调整指令调整所述无人机预设位置的姿态, 能够实吋 监控无人机各位置的姿态情况, 并进行各位置的姿态调整, 使无人机姿态保持 更精准。 [0074] As described above, a UAV attitude maintaining method according to an embodiment of the present invention acquires compensation data measured by a compensation sensor by acquiring position data of a preset position of the UAV measured by the attitude sensor, according to the position data and The compensation data calculates an attitude angle, receives a posture adjustment instruction of the user, adjusts a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction, and can effectively monitor each position of the drone Attitude situation, and posture adjustment of each position to maintain the attitude of the drone More precise.
[0075] 上述详细阐述了本发明实施例的方法, 下面为了便于更好地实施本发明实施例 的上述方案, 相应地, 下面还提供用于配合实施上述方案的装置。  The method of the embodiments of the present invention has been described in detail above. In order to facilitate the better implementation of the above embodiments of the embodiments of the present invention, correspondingly, an apparatus for implementing the above solutions is provided below.
[0076] 参阅图 4, 图 4为本发明实施例提供的一种无人机姿态保持装置的结构示意图, 所述装置应用于无人机, 所述装置 400包括以下功能模块: Referring to FIG. 4, FIG. 4 is a schematic structural diagram of a UAV attitude maintaining device according to an embodiment of the present invention. The device is applied to a UAV, and the device 400 includes the following functional modules:
[0077] 第一获取模块 410, 用于获取姿态传感器测量的无人机的预设位置的位置数据[0077] The first obtaining module 410 is configured to acquire location data of a preset position of the drone measured by the attitude sensor
, 其中, 所述姿态传感器至少有两个, 所述姿态传感器位于所述无人机的不同 位置。 The attitude sensor has at least two, and the attitude sensor is located at different positions of the drone.
[0078] 所述姿态传感器为组合式传感器, 由陀螺仪和加速度传感器组成。 其中, 所述 陀螺仪为传感陀螺仪, 输出角速度, 对所述角速度进行积分能得到角度, 由于 所述陀螺仪在零输入状态吋仍有输出, 它的输出是白噪声和慢变随机函数的叠 力口, 受此影响, 在积分的过程中, 会引进累计误差, 积分吋间越长, 误差就越 大。 因此, 需要利用加速度传感器来对陀螺仪进行校正, 所述加速度传感器利 用力的分解原理, 通过重力加速度在不同轴向上的分量来判断倾角, 没有积分 误差, 可以有效校正陀螺仪的误差。  [0078] The attitude sensor is a combined sensor composed of a gyroscope and an acceleration sensor. Wherein, the gyroscope is a sensing gyroscope, and outputs an angular velocity, and the angle is integrated to obtain an angle. Since the gyroscope still outputs in a zero input state, its output is a white noise and a slowly varying random function. The stacking force is affected by this. In the process of integration, the cumulative error will be introduced. The longer the integral time, the larger the error. Therefore, it is necessary to use an acceleration sensor to correct the gyroscope. The acceleration sensor uses the force decomposition principle to determine the tilt angle by the component of the gravity acceleration in different axial directions. Without the integral error, the error of the gyroscope can be effectively corrected.
[0079] 所述姿态传感器至少有两个, 且位于所述无人机的不同位置, 所述姿态传感器 的具体位置根据所述无人机的具体情况确定。 在一具体的实施例中, 若无人机 为四轴无人飞行器, 那么可以在所述无人机的四轴以及轴心上分别安装所述姿 态传感器, 对四轴无人飞行器不同的部位进行姿态监控。 在另一实施例中, 若 无人机为双翼无人飞机, 那么可以在所述无人机两边的侧翼上分别安装所述姿 态传感器。  [0079] The attitude sensors are at least two and located at different positions of the drone, and the specific position of the attitude sensor is determined according to the specific situation of the drone. In a specific embodiment, if the drone is a four-axis unmanned aerial vehicle, the attitude sensor may be separately mounted on the four axes and the axis of the drone, and the different parts of the four-axis unmanned aerial vehicle Perform posture monitoring. In another embodiment, if the drone is a two-wing unmanned aircraft, the attitude sensor can be mounted on each side of the drone.
[0080] 在本实施方式中, 所述位置数据为所述无人机预设位置的加速度、 角速度中的 至少一个, 其中, 所述加速度由所述姿态传感器中的加速度传感器测量得出, 所述角速度由所述姿态传感器中的陀螺仪测量得出。 在其他实施方式中, 所述 位置数据还可以包括所述预设位置距离地面的高度、 和地面控制系统的距离等 与所述预设位置相关的数据。  [0080] In the embodiment, the position data is at least one of an acceleration and an angular velocity of the preset position of the drone, wherein the acceleration is measured by an acceleration sensor in the attitude sensor, The angular velocity is measured by a gyroscope in the attitude sensor. In other embodiments, the location data may further include data related to the preset location, such as a height of the preset location from the ground, a distance from the ground control system, and the like.
[0081] 计算模块 420, 用于根据所述位置数据计算得出姿态角。  [0081] The calculation module 420 is configured to calculate an attitude angle according to the location data.
[0082] 在本实施方式中, 综合姿态传感器中的加速度传感器和陀螺仪的输出, 来计算 得出姿态角, 述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个, 所述俯仰 角、 滚转角、 偏航角分别是所述无人机的预设位置围绕 X、 Υ、 Ζ三个轴分别转 动形成的夹角, 所述俯仰角、 滚转角、 偏航角反映了所述无人机预设位置相对 地面的姿态。 [0082] In the present embodiment, the output of the acceleration sensor and the gyroscope in the attitude sensor is integrated to calculate Obtaining an attitude angle, wherein the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, wherein the pitch angle, the roll angle, and the yaw angle are respectively preset positions of the drone around X, Υ, The angle formed by the rotation of the three axes respectively, the pitch angle, the roll angle, and the yaw angle reflect the posture of the preset position of the drone relative to the ground.
[0083] 调整模块 430, 用于根据所述姿态角调整所述无人机预设位置的姿态。  [0083] The adjustment module 430 is configured to adjust a posture of the preset position of the drone according to the posture angle.
[0084] 在本实施方式中, 所述无人机在多种情况下都需要保持姿态, 例如, 当所述无 人机进行拍摄作业吋, 需要保持一定的姿态以使拍摄画面稳定; 当所述无人机 在天气状况恶劣的情况下, 在飞行吋需要保持一定的姿态以提高无人机的抗干 扰能力, 防止无人机损坏或失稳。  [0084] In the embodiment, the drone needs to maintain a posture in various situations. For example, when the drone performs a shooting operation, it is necessary to maintain a certain posture to stabilize the shooting image; In the case of bad weather conditions, the drone needs to maintain a certain posture during flight to improve the anti-interference ability of the drone and prevent the drone from being damaged or unstable.
[0085] 具体的, 若所述无人机预设位置的俯仰角过大, 则说明所述无人机预设位置相 对于水平面上下的幅度过大, 可以通过减小所述俯仰角来稳定所述预设位置的 姿态; 若所述无人机预设位置的滚转角过大, 则说明所述无人机预设位置翻转 的角度过大, 可以通过减小所述滚转角来稳定所述预设位置的姿态; 若所述无 人机预设位置的偏航角过大, 则说明所述无人机预设位置偏离了航线, 可以通 过调整使所述无人机预设位置按照正确的航线行进。  [0085] Specifically, if the pitch angle of the preset position of the drone is too large, it indicates that the preset position of the drone is too large relative to the horizontal plane, and may be stabilized by reducing the pitch angle. The attitude of the preset position; if the roll angle of the preset position of the drone is too large, it indicates that the angle of the preset position of the drone is too large, and the roll angle can be reduced to stabilize the The posture of the preset position; if the yaw angle of the preset position of the drone is too large, the preset position of the drone is deviated from the route, and the preset position of the drone may be adjusted according to the preset position The correct route travels.
[0086] 在本实施方式中, 所述无人机上不同的位置有不同的姿态传感器, 分别对不同 位置的姿态进行调整, 能够保持无人机每个位置的姿态, 进而保持无人机体的 姿态。  [0086] In the embodiment, different posture sensors are provided at different positions on the drone, and the postures of the different positions are respectively adjusted to maintain the posture of each position of the drone, thereby maintaining the posture of the unmanned body. .
[0087] 本发明实施例的一种无人机姿态保持装置 400能够实现如图 1所示的无人机姿态 保持方法, 具体请参阅图 1以及相关实施例, 此处不再重复赘述。  [0087] A UAV attitude maintaining device 400 according to an embodiment of the present invention can implement the UAV attitude maintaining method as shown in FIG. 1. For details, refer to FIG. 1 and related embodiments, and details are not described herein again.
[0088] 上述可知, 本发明实施例的一种无人机姿态保持装置通过获取姿态传感器测量 的无人机的预设位置的位置数据, 根据所述位置数据计算得出姿态角, 根据所 述姿态角调整所述无人机预设位置的姿态, 能够实吋监控无人机各位置的姿态 情况, 并进行各位置的姿态调整, 使无人机姿态保持更精准。  [0088] As described above, a UAV attitude maintaining device according to an embodiment of the present invention obtains a position angle according to a preset position of a UAV measured by an attitude sensor, and calculates an attitude angle according to the position data, according to the The posture angle adjusts the posture of the preset position of the drone, and can effectively monitor the posture of each position of the drone, and adjust the posture of each position, so that the posture of the drone is kept more precise.
[0089] 参阅图 5, 图 5为本发明实施例提供的另一种无人机姿态保持装置, 所述装置应 用于无人机, 所述装置 500和图 4所示装置 400的不同之处在于, 还包括以下功能 模块:  [0089] Referring to FIG. 5, FIG. 5 is another UAV attitude maintaining device according to an embodiment of the present invention. The device is applied to a UAV, and the difference between the device 500 and the device 400 shown in FIG. It also includes the following functional modules:
[0090] 第二获取模块 440, 用于获取补偿传感器测量的补偿数据, 其中, 所述补偿传 感器位于所述姿态传感器距离阈值内; [0090] a second obtaining module 440, configured to acquire compensation data measured by the compensation sensor, where the compensation transmission The sensor is located within the attitude sensor distance threshold;
[0091] 所述计算模块具体用于, 根据所述位置数据以及所述补偿数据计算得出姿态角  [0091] The calculation module is specifically configured to calculate a posture angle according to the position data and the compensation data
[0092] 在本实施方式中, 所述补偿传感器位于所述姿态传感器距离阈值内, 可以是在 所述姿态传感器的测量范围内等距离设置多个补偿传感器, 所述补偿传感器的 组成和所述姿态传感器相同, 用于测量所述补偿传感器所处位置的位置数据。 由于无人机飞行吋情况十分复杂, 所述补偿传感器提供的位置数据作为所述姿 态传感器测量出的位置数据的补偿数据, 通过补偿滤波处理, 能够计算得出更 加准确的姿态角。 [0092] In this embodiment, the compensation sensor is located within the attitude sensor distance threshold, and may be configured to equidistantly set a plurality of compensation sensors within the measurement range of the attitude sensor, the composition of the compensation sensor and the The attitude sensor is the same and is used to measure the position data of the position where the compensation sensor is located. Since the flight condition of the UAV is very complicated, the position data provided by the compensation sensor is used as the compensation data of the position data measured by the attitude sensor, and by the compensation filtering process, a more accurate attitude angle can be calculated.
[0093] 在本实施方式中, 综合所述姿态传感器和所述补偿传感器的输出, 来计算得出 姿态角, 述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个, 所述俯仰角、 滚转角、 偏航角分别是所述无人机的预设位置围绕 X、 Υ、 Ζ三个轴分别转动形 成的夹角, 所述俯仰角、 滚转角、 偏航角反映了所述无人机预设位置相对地面 的姿态。  [0093] In the present embodiment, the attitude angle is calculated by integrating the output of the attitude sensor and the compensation sensor, and the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle, the pitch The angle, the roll angle, and the yaw angle are respectively formed by the rotation of the preset positions of the drone around the X, Υ, and 轴 axes, and the pitch angle, the roll angle, and the yaw angle reflect the angle The position of the drone's preset position relative to the ground.
[0094] 接收模块 450, 用于接收用户的姿态调整指令;  [0094] The receiving module 450 is configured to receive a posture adjustment instruction of the user;
[0095] 所述调整模块具体用于, 根据所述姿态角以及所述姿态调整指令调整所述无人 机预设位置的姿态。  [0095] The adjustment module is specifically configured to adjust a posture of the preset position of the UAV according to the posture angle and the posture adjustment instruction.
[0096] 在本实施方式中, 用户可以通过控制终端, 例如无人机遥控器或者地面控制系 统对无人机发出姿态调整指令, 所述用户可以根据所述无人机飞行区域的实际 情况、 例如天气状况、 无人机数量、 地理情况等来对所述无人机发出姿态调整 指令, 以使所述无人机根据飞行区域的实际情况或者用户需求来调整飞行姿态  [0096] In this embodiment, the user may issue an attitude adjustment command to the drone through a control terminal, such as a drone remote controller or a ground control system, and the user may according to the actual situation of the flight area of the drone, For example, a weather condition, a number of drones, a geographical situation, etc., to issue an attitude adjustment command to the drone, so that the drone adjusts the flight attitude according to the actual situation of the flight area or the user's demand.
[0097] 在本实施方式中, 所述姿态角表明所述无人机的飞行姿态, 所述无人机上不同 的位置有不同的姿态传感器, 分别对不同位置的姿态进行调整, 能够保持无人 机每个位置的姿态, 进而保持无人机体的姿态, 同吋, 所述无人机根据用户发 送的姿态调整指令来调整姿态能够使所述无人机适应飞行环境和用户需求, 所 述无人机根据所述姿态角以及所述姿态调整指令进行调整能够更好地保持所述 无人机预设位置的姿态。 [0098] 可以理解的是, 本发明实施例的一种无人机姿态保持装置 500能够实现如图 3所 示的无人机姿态保持方法, 具体请参阅图 3以及相关实施例, 此处不再重复赘述 [0097] In the embodiment, the attitude angle indicates a flight attitude of the drone, and different posture sensors on the unmanned aerial vehicle have different attitude sensors, and respectively adjust attitudes of different positions to maintain an unmanned position. The posture of each position of the machine, thereby maintaining the posture of the unmanned body, and the unmanned aerial vehicle adjusting the posture according to the posture adjustment command sent by the user can adapt the drone to the flight environment and the user's demand, Adjusting the man-machine according to the posture angle and the posture adjustment command can better maintain the posture of the preset position of the drone. [0098] It can be understood that the UAV posture maintaining device 500 of the embodiment of the present invention can implement the UAV attitude maintaining method as shown in FIG. 3, and specifically refer to FIG. 3 and related embodiments, where Repeat
[0099] 上述可知, 本发明实施例的一种无人机姿态保持装置通过获取姿态传感器测量 的无人机的预设位置的位置数据, 获取补偿传感器测量的补偿数据, 根据所述 位置数据以及所述补偿数据计算得出姿态角, 接收用户的姿态调整指令, 根据 所述姿态角以及所述姿态调整指令调整所述无人机预设位置的姿态, 能够实吋 监控无人机各位置的姿态情况, 并进行各位置的姿态调整, 使无人机姿态保持 更精准。 [0099] As described above, a UAV attitude maintaining device according to an embodiment of the present invention acquires compensation data measured by a compensation sensor by acquiring position data of a preset position of the UAV measured by the attitude sensor, according to the position data and The compensation data calculates an attitude angle, receives a posture adjustment instruction of the user, adjusts a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction, and can effectively monitor each position of the drone Attitude situation, and posture adjustment of each position, so that the attitude of the drone is kept more precise.
[0100] 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, 该程序在执行吋, 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  [0100] Those skilled in the art can understand that all or part of the process of implementing the above embodiments may be completed by a computer program to instruct related hardware, and the program may be stored in a computer readable storage medium. The program, after execution, may include the flow of an embodiment of the methods as described above. The storage medium may be a magnetic disk, an optical disk, or a read-only storage memory (Read-Only)
Memory , ROM) 或随机存储记忆体 (Random Access Memory , RAM) 等。  Memory, ROM) or Random Access Memory (RAM).
[0101] 以上所揭露的仅为本发明一种较佳实施例而已, 当然不能以此来限定本发明之 权利范围, 本领域普通技术人员可以理解实现上述实施例的全部或部分流程, 并依本发明权利要求所作的等同变化, 仍属于发明所涵盖的范围。  The above disclosure is only a preferred embodiment of the present invention, and of course, the scope of the present invention is not limited thereto, and those skilled in the art can understand all or part of the process of implementing the above embodiments, and Equivalent variations of the claims of the invention are still within the scope of the invention.
技术问题  technical problem
问题的解决方案  Problem solution
发明的有益效果  Advantageous effects of the invention

Claims

权利要求书 Claim
[权利要求 1] 一种无人机姿态保持方法, 其特征在于, 包括:  [Attach 1] A method for maintaining a posture of a drone, comprising:
获取姿态传感器测量的无人机的预设位置的位置数据, 其中, 所述姿 态传感器至少有两个, 所述姿态传感器位于所述无人机的不同位置; 根据所述位置数据计算得出姿态角;  Obtaining position data of a preset position of the drone measured by the attitude sensor, wherein the attitude sensor has at least two, the posture sensor is located at different positions of the drone; and calculating a posture according to the position data Horn
根据所述姿态角调整所述无人机预设位置的姿态。  Adjusting the posture of the preset position of the drone according to the posture angle.
[权利要求 2] 根据权利要求 1所述的方法, 其特征在于, 所述位置数据为所述无人 机预设位置的加速度、 角速度中的至少一个。  [Claim 2] The method according to claim 1, wherein the position data is at least one of an acceleration and an angular velocity of the preset position of the UAV.
[权利要求 3] 根据权利要求 1所述的方法, 其特征在于, 所述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个。 [Claim 3] The method according to claim 1, wherein the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle.
[权利要求 4] 根据权利要求 1所述的方法, 其特征在于, 在所述根据所述位置数据 计算得出姿态角之前, 还包括: [Claim 4] The method according to claim 1, wherein before the calculating the posture angle according to the position data, the method further includes:
获取补偿传感器测量的补偿数据, 其中, 所述补偿传感器位于所述姿 态传感器距离阈值内;  Acquiring compensation data measured by the compensation sensor, wherein the compensation sensor is located within the attitude sensor distance threshold;
所述根据所述位置数据计算得出姿态角具体为: 根据所述位置数据以及所述补偿数据计算得出姿态角。  The calculating the attitude angle according to the position data is specifically: calculating an attitude angle according to the position data and the compensation data.
[权利要求 5] 根据权利要求 1所述的方法, 其特征在于, 在所述根据所述姿态角调 整所述无人机预设位置的姿态之前, 还包括: [Claim 5] The method according to claim 1, wherein before the adjusting the posture of the preset position of the drone according to the posture angle, the method further includes:
接收用户的姿态调整指令;  Receiving a posture adjustment instruction of the user;
所述根据所述姿态角调整所述无人机预设位置的姿态具体为: 根据所述姿态角以及所述姿态调整指令调整所述无人机预设位置的姿 态。  The adjusting the posture of the preset position of the drone according to the posture angle is specifically: adjusting an attitude of the preset position of the drone according to the posture angle and the posture adjustment instruction.
[权利要求 6] —种无人机姿态保持装置, 其特征在于, 包括:  [Claim 6] A UAV attitude maintaining device, comprising:
第一获取模块, 用于获取姿态传感器测量的无人机的预设位置的位置 数据, 其中, 所述姿态传感器至少有两个, 所述姿态传感器位于所述 无人机的不同位置;  a first acquiring module, configured to acquire position data of a preset position of the drone measured by the attitude sensor, where the at least two posture sensors are located at different positions of the drone;
计算模块, 用于根据所述位置数据计算得出姿态角;  a calculation module, configured to calculate an attitude angle according to the position data;
调整模块, 用于根据所述姿态角调整所述无人机预设位置的姿态。 And an adjustment module, configured to adjust a posture of the preset position of the drone according to the posture angle.
[权利要求 7] 根据权利要求 6所述的装置, 其特征在于, 所述位置数据为所述无人 机预设位置的加速度、 角速度中的至少一个。 [Clave 7] The apparatus according to claim 6, wherein the position data is at least one of an acceleration and an angular velocity of the preset position of the UAV.
[权利要求 8] 根据权利要求 6所述的装置, 其特征在于, 所述姿态角包括俯仰角、 滚转角、 偏航角中的至少一个。 [Claim 8] The apparatus according to claim 6, wherein the attitude angle includes at least one of a pitch angle, a roll angle, and a yaw angle.
[权利要求 9] 根据权利要求 6所述的装置, 其特征在于, 还包括: [Claim 9] The device according to claim 6, further comprising:
第二获取模块, 用于获取补偿传感器测量的补偿数据, 其中, 所述补 偿传感器位于所述姿态传感器距离阈值内;  a second acquiring module, configured to acquire compensation data of the compensation sensor measurement, where the compensation sensor is located within the attitude sensor distance threshold;
所述计算模块具体用于, 根据所述位置数据以及所述补偿数据计算得 出姿态角。  The calculation module is specifically configured to calculate an attitude angle according to the position data and the compensation data.
[权利要求 10] 根据权利要求 6所述的装置, 其特征在于, 还包括:  [Claim 10] The device according to claim 6, further comprising:
接收模块, 用于接收用户的姿态调整指令;  a receiving module, configured to receive a posture adjustment instruction of the user;
所述调整模块具体用于, 根据所述姿态角以及所述姿态调整指令调整 所述无人机预设位置的姿态。  The adjustment module is specifically configured to adjust a posture of the preset position of the drone according to the posture angle and the posture adjustment instruction.
PCT/CN2017/073112 2016-12-06 2017-02-08 Method and device for maintaining attitude of unmanned aerial vehicle WO2018103192A1 (en)

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