CN112896534B - Control method, controller and manned aircraft - Google Patents
Control method, controller and manned aircraft Download PDFInfo
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
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- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05B—CONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
- G05B19/00—Programme-control systems
- G05B19/02—Programme-control systems electric
- G05B19/04—Programme control other than numerical control, i.e. in sequence controllers or logic controllers
Abstract
The application discloses a control method for a manned aircraft, comprising the following steps: the method comprises the steps of obtaining data of the manned aircraft, carrying out classification processing on the data according to a preset category, generating corresponding display information, and controlling a display device of the manned aircraft to display the corresponding classified display information in a preset area. Therefore, data can be managed in a unified mode, communication transmission work among the modules is reduced to a certain extent, and therefore the coupling degree among the modules is reduced. And the data is uniformly classified according to the preset categories and is subjected to different classification according to different display screens, so that each display device can display the display information which is classified correspondingly in the preset area. The application also discloses a controller and a manned aircraft.
Description
Technical Field
The application relates to the technical field of manned aircrafts, in particular to a control method, a controller and a manned aircraft.
Background
As an emerging vehicle, the manned aircraft has the related technology which is rapidly developing and perfecting. In order to ensure the safe operation of the manned aircraft, the relevant data of the manned aircraft can be comprehensively provided for the user in the flight process so as to facilitate the user to effectively operate in time. How to effectively provide data of manned aircrafts for drivers and passengers becomes a problem to be solved urgently.
Disclosure of Invention
In view of the above, the present application is directed to solving, at least to some extent, one of the problems in the related art. Therefore, the application aims to provide a control method, a controller and a manned aircraft.
The embodiment of the application provides a control method, which is used for a manned aircraft and comprises the following steps:
acquiring data of the manned aircraft;
classifying the data according to a preset category and generating corresponding display information;
and controlling a display device of the manned aircraft to display the display information of the corresponding classification in a preset area.
In some embodiments, said controlling the display device of the manned aircraft to display the display information of the corresponding category in the predetermined area includes:
and controlling the preset area of the display device to display the display information of the corresponding classification in a preset display style.
The application also provides a controller for manned vehicle, manned vehicle still include with display device that the controller is connected, the controller is used for:
acquiring data of the manned aircraft;
classifying the data according to a preset category and generating corresponding display information;
and controlling the display device to display the display information of the corresponding classification in a preset area.
In some embodiments, the controller is further configured to control the predetermined area of the display device to display the display information of the corresponding category in a predetermined display style.
In some embodiments, the controller includes a first circuit board and a second circuit board electrically connected to the first circuit board, the first circuit board is configured to acquire the data and transmit the data to the second circuit board, the second circuit board is configured to classify the data according to predetermined categories and generate corresponding display information, and is configured to control the display device to display the corresponding classified display information in a predetermined area, where the predetermined categories include attitude data, status data, signal data, cabin status data, and/or navigation map data.
In some embodiments, the manned aircraft includes a flight control system configured to collect attitude data of the manned aircraft, the first circuit board includes a first communication interface to communicatively couple with the flight control system, the first circuit board obtains the attitude data via the first communication interface, wherein the attitude data includes roll and/or pitch angles of the manned aircraft.
In some embodiments, the first circuit board comprises a second communication interface to connect with a plurality of communication modules of the manned aircraft, and the first circuit board acquires signal data of the manned aircraft collected by the plurality of communication modules through the second communication interface, wherein the signal data comprises communication signal data of a plurality of wireless communication signals and/or data transmission stations;
the signal data further comprises GPS data of the manned aircraft, the flight control system is further used for collecting the GPS data, and the first circuit board acquires the GPS data through the first communication interface.
In certain embodiments, the status data comprises speed status data, altitude status data, temperature data, and/or power status data of the manned aircraft, the flight control system is further configured to collect status data of the manned aircraft, the first circuit board obtains the status data via the first communication interface, the status data comprises speed status data and/or altitude status data of the manned aircraft, wherein the speed status data comprises a lifting speed and/or a flying speed, and the altitude status data comprises a barometric altitude and/or a radar altitude;
the first circuit board comprises a third communication interface so as to be connected with a motor module and an electric regulation module of the manned aircraft;
the first circuit board comprises a fourth communication interface to be connected with a power module of the manned aircraft, the first circuit board acquires power battery electric quantity data of the power module through the third communication interface and the fourth communication interface to determine the power state data, the power state data further comprises electric quantity data of a flight control system, and the first circuit board acquires the electric quantity data of the flight control system through the first communication interface;
the first circuit board acquires temperature data of the motor module and the electric regulation module through the third communication interface and the fourth communication interface.
In some embodiments, the navigation map data includes longitude and latitude data of the manned vehicle, the flight control system is further configured to collect the longitude and latitude data of the manned vehicle, and the first circuit board obtains the longitude and latitude data through the first communication interface to obtain the navigation map data.
In some embodiments, the navigation map data further includes map data, and the second circuit board is further configured to perform a fusion process on the longitude and latitude data and the map data to display the data through the display device.
In some embodiments, the cockpit status data includes door status data, lamp status data, and/or ground air status data, the first circuit board includes a fifth communication interface to interface with a cockpit sensor of the manned aircraft, and the first circuit board obtains the cockpit status data of the manned aircraft through the fifth communication interface.
In some embodiments, the predetermined category further includes alarm information, and the second circuit board is further configured to parse the data to generate the alarm information when there is an anomaly in the data.
The application also provides a manned aircraft, which comprises the controller in any one of the above.
The present application also provides a non-transitory computer-readable storage medium of a computer program, which when executed by one or more processors, implements the control method of any one of the above.
In the implementation mode of the application, the data can be managed in a unified mode by intensively acquiring part or all data of the manned aircraft, communication transmission work among the modules is reduced to a certain extent, and therefore the coupling degree among the modules is reduced. And classifying the data according to the preset category to generate corresponding display information, and controlling a display device of the manned aircraft to display the corresponding classified display information in a preset area. Because the manned aircraft has the characteristic of multiple display devices, different seats need to display different contents. The data are classified uniformly according to the preset category and are classified differently according to different display screens, so that each display device can display the display information classified correspondingly in the preset area. The manned vehicle has high requirements on safety data, the safety data need to be processed in a unified mode through the modules, and the safety data of the modules can be collected and classified and then further sent to the expanded processor to be analyzed and returned. The centralized collection and classification processing of the data are beneficial to the realization of subsequent services.
Drawings
The above and/or additional aspects and advantages of the present application will become apparent and readily appreciated from the following description of the embodiments, taken in conjunction with the accompanying drawings of which:
fig. 1 is a schematic flow chart of a control method according to an embodiment of the present application;
FIG. 2 is a schematic structural diagram of a controller according to an embodiment of the present application;
FIG. 3 is a schematic flow chart of a control method according to an embodiment of the present application;
FIG. 4 is a schematic structural diagram of a controller according to an embodiment of the present application;
FIG. 5 is a schematic structural diagram of a controller according to an embodiment of the present application;
FIG. 6 is a schematic structural diagram of a controller according to an embodiment of the present application;
FIG. 7 is a schematic structural diagram of a controller according to an embodiment of the present application;
FIG. 8 is a schematic structural diagram of a controller according to an embodiment of the present application;
fig. 9 is an exemplary view of a display device according to an embodiment of the present application;
fig. 10 is a schematic structural diagram of a controller according to an embodiment of the present application.
Detailed Description
Reference will now be made in detail to embodiments of the present application, examples of which are illustrated in the accompanying drawings, wherein like reference numerals refer to the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary only for explaining the present application and are not to be construed as limiting the present application.
In the description of the present application, it is to be understood that the terms "first", "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance or implying any number of technical features indicated. Thus, features defined as "first", "second", may explicitly or implicitly include one or more of the described features. In the description of the present application, "a plurality" means two or more unless specifically limited otherwise.
Referring to fig. 1, an embodiment of the present application provides a control method for a manned aircraft, the control method including:
s10: acquiring data of the manned aircraft;
s20: classifying the data according to a preset category and generating corresponding display information;
s30: and controlling a display device of the manned aircraft to display the display information corresponding to the classification in a predetermined area.
Referring to fig. 2, the present embodiment further provides a controller 100 for a manned vehicle. The manned vehicle also includes a display device 200 connected to the controller 100. The controller 100 is configured to obtain data of the manned vehicle, classify the data according to a predetermined category, generate corresponding display information, and control the display device 200 of the manned vehicle to display the corresponding classified display information in a predetermined area.
Referring to fig. 2 again, the present embodiment further provides a manned vehicle 1000, where the manned vehicle 1000 includes the controller 100 and the display devices 200 according to the present embodiment.
The embodiment of the application also provides the electronic equipment. The server includes a memory and a processor. The memory has stored therein a computer program, and the processor is configured to acquire data of the manned vehicle 1000, classify the data according to a predetermined classification, generate corresponding display information, and control the display device 200 of the manned vehicle 1000 to display the display information corresponding to the classification in a predetermined area.
As an emerging vehicle, the technology related to the manned aircraft is rapidly developing and perfecting. The manned aircraft comprises a flying automobile, can fly in the air or run on the land, and can be switched between a flight mode and a land mode at any time according to the requirements of users. Compared with automobiles and airplanes, the flying automobile has more systems, modules, functions, data and display systems. Among these, the cockpit system of an aircraft has huge data, including dynamic data and static data. Users often need to acquire partial data such as flight status data, safety data and the like in real time and display the required data or status in real time through equipment such as a display screen and the like.
The controller 100 of the embodiment of the present application may acquire data of the manned vehicle 1000. Wherein the controller 100 includes a plurality of chips or a circuit board including a plurality of chips. The data of the manned vehicle 1000 includes part or all of the data of the manned vehicle 1000, such as data of a cockpit system of the manned vehicle 1000, flight status data, flight attitude data, and the like, specifically according to the processing capability or business requirements of the controller 100. The function of the controller 100 is to collectively acquire or collect data of a plurality of modules or devices, and the controller 100 may actively collect data of the plurality of modules or devices and may passively receive data transmitted by the plurality of modules or devices. The specific data content thereof should not be construed as limiting the application.
Further, after the controller 100 acquires the data of the manned vehicle 1000, the data is classified according to a predetermined category and corresponding display information is generated. The preset category is a preset data category, such as a manned vehicle state data category, a navigation map data category and the like. The predetermined categories may be set based on the data requirements of the display area of the display device 200, and if the electric quantity area can display the electric quantity of the flight control system and the electric quantity of the power module, the electric quantity of the flight control system and the electric quantity of the power module are classified into the predetermined categories of the electric quantity. Or setting a predetermined category based on the function, such as the flight control system function, classifying all data collected from the flight control system into the predetermined category of the flight control system.
The data classification processing comprises the step of classifying the data of a single module or the step of fusing and classifying the data of a plurality of modules. It will be appreciated that manned vehicles differ from automobiles and airplanes and that the type of data required varies and changes in real time. The manner in which the classification is handled by the controller 100 is different, as is the data collected and displayed for the flight mode and the land mode. In addition, the classification process includes but is not limited to splitting, combining, and the like. For example, the data collected by a single module can be divided into a plurality of predetermined categories, or the data collected by a plurality of modules can be combined into one predetermined category, or the division and the combination can be performed simultaneously.
In some embodiments, the classification process further includes filtering according to the data range of the business application, such as the current working mode, to remove useless data or abnormal data that cannot be used normally. The process may then be de-duplicated, and multiple modules may return duplicate data, which may be culled. And then carrying out further classification processing on the preprocessed data. For example, when the controller 100 receives the current flight mode, it switches to the processing and display mode of the flight mode. The vehicle state data of the land mode can be culled during preprocessing.
In some embodiments, the collected data may also be input into a machine learning model, such as a logistic regression analysis model, for prediction. Such as predictions of time of flight, etc., the predicted data may be displayed by the display device 200.
Further, the corresponding display information is generated after the data classification processing is completed, and then the display device 200 of the manned aircraft 1000 is controlled to display the display information of the corresponding classification in a predetermined area. The display device 200 includes a plurality of display screens, such as a driving display screen, a passenger driving display screen, and a micro-size display screen. And miniature size displays include many sizes such as 5 inch displays. The display device 200 is intended to display data classified and processed by the controller 100. The controller 100 may send different data to the corresponding display device 200 for displaying, or send the same data to different display devices 200 for displaying, specifically, according to the service requirement. Accordingly, different display devices 200 may also display the same data content, for example, the front-driving display screen and the front-driving display screen may display the same content.
The predetermined regions of the display device 200 are a plurality of display regions of the GUI interface, such as a flight speed display region that displays the instantaneous flight speed of the current manned aircraft 1000. The predetermined categories of the controller 100 may be classified according to predetermined regions of the display device 200. It is understood that different display devices 200 have different predetermined regions, and the controller 100 may perform corresponding classification processing according to the connected different display devices 200, or may perform further classification processing on the data through an extended processor.
Therefore, in the embodiment of the application, the data can be uniformly managed by intensively acquiring part or all data of the manned aircraft, and the communication transmission work among the modules is reduced to a certain extent, so that the coupling degree among the modules is reduced. And classifying the data according to the preset categories, generating corresponding display information, and controlling a display device of the manned aircraft to display the display information corresponding to the categories in a preset area. Because the manned aircraft has the characteristic of multiple display devices, different seats need to display different contents. The data are classified uniformly according to the preset category and are classified differently according to different display screens, so that each display device can display the display information classified correspondingly in the preset area. And manned vehicle is higher to the demand of safety class data, and safety class data need a plurality of modules to carry out unified processing, and this application can make the safe data acquisition and the categorised back of a plurality of modules, can further send the treater of extension to carry out data analysis and return again. The centralized collection and classification processing of the data are beneficial to the realization of subsequent services.
Referring to fig. 3, in some embodiments, S30 includes:
s31: and controlling a predetermined area of the display device to display the display information of the corresponding classification in a predetermined display style.
In some embodiments, the controller 100 is further configured to control a predetermined region of the display device to display the display information of the corresponding category in a predetermined display style.
In some embodiments, the processor is configured to control a predetermined area of the display device to display the display information of the corresponding category in a predetermined display style.
The display device may include a variety of display styles, such as a reduced mode, or a detailed mode, etc. And the displayed area can be customized according to the user. The second circuit board 20 may control a predetermined region of the display device 200 to display the display information of the corresponding category in a predetermined display style according to a plurality of display styles.
Referring to fig. 4, in some embodiments, the controller 100 includes a first circuit board 10 and a second circuit board 20 electrically connected to the first circuit board 10, the first circuit board 10 is configured to acquire data and transmit the data to the second circuit board 20, the second circuit board 20 is configured to classify the data according to predetermined categories and generate corresponding display information, and is configured to control the display device 200 to display the corresponding classified display information in a predetermined area, where the predetermined categories include attitude data, status data, signal data, cabin status data, and/or navigation map data.
The controller 100 for the manned aircraft 1000 comprises a first circuit board 10 and a second circuit board 20, wherein the first circuit board 10 is electrically connected with the second circuit board 20. The physical connection between the first circuit board 10 and the second circuit board 20 can be achieved by means of pins, for example, the second circuit board 20 is inserted on the first circuit board 10, and the first circuit board 10 can be used as an extension board of the second circuit board 20. Wherein, the first circuit board 10 and the second circuit board 20 may each include a single chip or a plurality of chips or a circuit board including a plurality of chips. In some embodiments, the first circuit board 10 and the second circuit board 20 may be integrated into one body.
Specifically, the first circuit board 10 is used for acquiring data of the manned aircraft, and processing and transmitting the data to the second circuit board 20. The obtaining mode of the first circuit board 10 includes real-time active acquisition or active input of an external device, and the specific mode is set according to data and a device type. For example, the current pitch angle, roll angle, etc. of the manned vehicle 1000 may be set to active acquisition, and when the manned vehicle 1000 is switched to the flight mode, the current pitch angle, roll angle, etc. may be set to periodic acquisition. For example, the electric quantity data can be actively input into the first circuit board 10 through a battery, a motor, an electric regulator and other devices according to changes, and the first circuit board 10 can further calculate the current real-time electric quantity of the manned aircraft 1000.
When the first circuit board 10 acquires data of the manned vehicle 1000, the data is transmitted to the second circuit board 20. The second board 20 receives the data and then further classifies the data according to a predetermined classification. The first circuit board 10 collects dynamic and static data of a plurality of modules, the collected data come from different modules, and the data are related to each other, and particularly for displaying certain states, the data of the plurality of modules need to be collected. For example, the electric quantity display needs the data of the battery module, the motor module and the electric regulation module. It will be appreciated that the type of data required by the manned aircraft 1000 in the different modes of operation may change in real time. The classification is handled differently, as the flight mode and the land mode require different data to be collected and displayed. The second circuit board 20 of the controller 100 may perform corresponding processing on the received collected data according to different operation modes.
In some embodiments, the second circuit board 20 may pre-process the received data, i.e., perform screening according to a preset available data range to remove useless data or abnormal data that cannot be used normally. The process may then be de-duplicated, and multiple modules may return duplicate data, which may be culled. For example, when the controller 100 receives the current flight mode, it switches to the processing and display mode of the flight mode. The vehicle state data of the land mode can be culled during preprocessing.
And further, classifying the preprocessed data according to a preset category. The predetermined categories include attitude data, status data, signal data, cockpit status data, and/or navigation map data. The attitude data of the manned aircraft are used for describing the state data of three axes of the manned aircraft in the air relative to a certain reference line or a certain reference plane or a certain fixed coordinate system, such as roll angle, pitch angle and the like. The state data includes data on the current state of manned aircraft 1000, such as speed state, power state, altitude state, and the like. The signal data includes data on the status of the signal that the manned vehicle 1000 is currently in communication with a radio or satellite, such as the GPS satellite health status. The cabin status data includes data of the cabin of the manned aircraft 1000, such as door, navigation lights, etc. The navigation map data includes navigation information, map display, and the like of the manned vehicle 1000.
In some embodiments, the collected data may be input into a machine learning model, such as a logistic regression analysis model, or the like, for prediction. Such as predictions of time of flight, etc. The predicted data may be displayed by the display device 200.
When the second circuit board 20 completes the data processing, display information is generated, and then the display device 200 is controlled to display the display information of the corresponding category in a predetermined area. The display device 200 includes a plurality of display screens, such as a driving display screen, a passenger driving display screen, and a micro-size display screen. Wherein the micro-sized display screen includes a variety of sizes such as a 5 inch display screen. The display device 200 is intended to display data processed by the second circuit board 20. The second circuit board 20 may send different data to the corresponding display device 200 for displaying, or send the same data to different display devices 200 for displaying, specifically, set according to business requirements. The different display devices 200 may also display the same data content, for example, the driving display screen and the assistant driving display screen may display the same content. Further, when the user changes the display mode of the display device 200, the second circuit board 20 may change the data processing mode according to the preset mode.
It should be noted that the controller 100 of the present application includes a first circuit board 10 for acquiring data of the manned vehicle, and a second circuit board 20 for processing and generating display information data. In some embodiments, the functions of acquisition and processing may be located on the first circuit board 10, while the second circuit board 20 is used to transmit the processed data to the display device 200 for display. The data acquisition, processing and display can be distributed to different chips according to the processing capacity of the chips.
In this way, the controller 100 for the manned vehicle 1000 of the present application acquires the data of the manned vehicle by using the first circuit board 10 and transmits the data to the second circuit board 20, and simultaneously processes the data by using the second circuit board 20 to generate the display information, so as to display the generated display information through the display device 200. The dynamic data and the static data generated by the manned vehicle 1000 in various working modes can be collected, the data are classified and processed, and the data are sent to the display devices 200 for classified display. Meanwhile, as the manned aircraft has huge data volume, the acquisition input, processing and display output functions are respectively realized by using processors such as different chips, and the processing performance of the controller can be effectively improved. Further, for collection of each of multiple modules in the prior art, data collection is unified to the first circuit board 10, unified management can be performed on data, communication transmission work among the modules is reduced to a certain extent, and therefore the coupling degree among the modules is reduced.
Referring to fig. 5, in some embodiments, manned vehicle 1000 further includes a flight control system 300, flight control system 300 is configured to collect attitude data of manned vehicle 100, first circuit board 10 includes a first communication interface a for communicating with flight control system 300, and first circuit board 10 obtains attitude data through first communication interface a, where the attitude data includes roll angle and/or pitch angle of the manned vehicle.
Specifically, flight control system 300 is primarily designed to ensure stability and maneuverability of manned vehicle 1000, enhance flight safety and reduce pilot workload, including aircraft pitch, roll and yaw control, lift and drag control, manual trim, direct force control, and other configuration changes such as changing wing sweep, horizontal stabilizer angle, etc. Attitude data for the manned vehicle 1000, including roll and/or pitch angles of the manned vehicle, may be collected by the flight control system 300.
Further, the first circuit board 10 includes a first communication interface a including a plurality of 232 interfaces. The first circuit board 10 may be communicatively connected to a plurality of modules of the flight control system 300 through the first communication interface a, so as to acquire attitude data.
It should be noted that the attitude data of the manned vehicle may vary according to the form of the manned vehicle, and the above data contents are described as examples. The purpose of the present application is to demonstrate that the present application can collect and classify attitude data of the manned vehicle 1000 by the controller 100. Attitude data for manned vehicle 1000 is data describing the state of the three axes of the manned vehicle in the air with respect to a reference line or plane, or a fixed coordinate system. Simple increases and decreases based on this range can be considered as simple alternatives to the present application.
Referring to FIG. 6, in some embodiments, manned aircraft 1000 also includes a plurality of communication modules 400, 410, 420. The first circuit board 10 includes a second communication interface B to connect with the plurality of communication modules 400, 410, 420, etc. of the manned aircraft 1000, and the first circuit board 10 acquires signal data of the manned aircraft 1000 collected by the plurality of communication modules 400, 410, 420, etc. through the second communication interface B, where the signal data includes communication signal data of a plurality of wireless communication signals and/or data transfer stations.
The plurality of communication modules comprise a 5G communication module, a 4G communication module, a 2.4G communication module, a data transmission radio module and the like. The manned vehicle 1000 acquires wireless communication data such as audio and video, images, characters and other information in real time through each communication module. The plurality of communication modules may be external to the first circuit board 10 or may be embedded in the first circuit board 10. When a plurality of communication modules are externally connected to the first circuit board 10, the second communication interface B includes an extended GPIO interface such as a 15-port GPIO interface.
The first circuit board 10 obtains signal data of the manned vehicle 1000 collected by the plurality of communication modules through the first communication interface B, where the signal data includes communication signal data of a plurality of wireless communication signals such as 5G communication signals, 4G communication signals, 2.4G communication signal lamps, and/or data transmission radio stations.
Further, the signal data also includes GPS data of the manned vehicle 1000. Wherein flight control system 300 includes a GPS module. The first circuit board 30 obtains GPS data from the flight control system 300 through the first communication interface a.
It should be noted that the signal data of the manned vehicle may vary according to different communication systems, and the above data contents are only described as examples. The purpose of the present application is to demonstrate that the present application can collect and classify signal data of the manned vehicle 1000 by the controller 100. The signal data of the manned vehicle 1000 is used for transmission data when the manned vehicle communicates with the outside. Simple increases and decreases based on this range can be considered as simple alternatives to the present application.
Referring to fig. 7, in some embodiments, the manned aircraft 1000 further includes a motor module 500, an electric tilt module 600, and a power module 700.
The status data includes speed status data, altitude status data, temperature data, and/or power status data of manned aircraft 1000.
The first circuit board 10 further includes a third communication interface C to connect with the electric motor module 500 and the electric tilt module 600 of the manned aircraft 1000. The first circuit board 10 further comprises a fourth communication interface D for connection with a power module 700 of the manned aircraft 1000. The third communication interface C includes CAN interfaces, and the CAN interfaces include CAN1 and CAN2 interfaces according to different communication objects, and the number of the CAN interfaces is not limited. In this embodiment, CAN1 is connected with motor module 500, and CAN2 is connected with electrical tilt module 600. The fourth communication interface D includes a plurality of 485 interfaces, which are respectively connected to a plurality of power modules of the manned vehicle 1000.
The first circuit board 10 acquires power battery power data of the power module 700 through the third communication interface C and the fourth communication interface D to determine power state data, the power state data further includes power data of the flight control system, and the first circuit board 10 acquires the power data of the flight control system 300 through the first communication interface a.
The first circuit board 10 obtains temperature data of the electric motor module 500 and the electric tilt module 600 through the third communication interface C and the fourth communication interface D.
Further, after the first circuit board 10 acquires the state data of the manned aircraft, the state data is sent to the second circuit board 20 for classification. If the electric quantity data of the power battery collected by the third communication interface C and the fourth communication interface D and the electric quantity data of the flight control system 300 collected by the first communication interface a are classified as the electric quantity reservation.
It should be noted that the state data of the manned vehicle is huge, and the data content is described as an example. The purpose of the present application is to demonstrate that the present application can collect and classify status data of the manned vehicle 1000 via the controller 100. The state data of the manned aircraft are used for describing the states of the manned aircraft such as the power, the speed, the altitude and the like of the current flight or driving. Simple increases and decreases based on this range can be considered as simple alternatives to the present application.
In some embodiments, the navigation map data includes longitude and latitude data of the manned vehicle 1000, the flight control system 300 is further configured to collect the longitude and latitude data of the manned vehicle 1000, and the first circuit board 10 acquires the longitude and latitude data through the first communication interface a to obtain the navigation map data.
The flight control system 300 includes data related to a navigation module, and the first circuit board 10 acquires latitude and longitude data, i.e., real-time navigation coordinates of the manned vehicle 1000, including a terrestrial coordinate system and/or an airport coordinate system, from the flight control system 300 through the first communication interface a. Navigation map data is used to describe the current location information of manned vehicle 1000, so simple addition or subtraction based on this range may be considered a simple alternative to the present application.
In some embodiments, the navigation map data further includes map data, and the second circuit board 20 is further configured to perform a fusion process of the longitude and latitude data and the map data for displaying through the display device 200.
Specifically, the map data may be placed in a communication module, such as a 4G communication module, and the second circuit board 20 acquires real-time or offline map data through the 4G communication module, and fuses longitude and latitude data acquired by the first communication interface a from the flight control system 300 to obtain the current geographic position information of the manned aircraft 1000.
Further, the second circuit board 20 sends the data obtained by fusing the longitude and latitude data and the map data to the navigation area of the display device 200 for display, and the display device 200 can display the current position of the manned vehicle 1000, the position of the manned vehicle and the geographic information in a certain range around the manned vehicle, such as the place name and the building information.
Referring to FIG. 8, in some embodiments, manned aircraft 1000 further includes a cockpit sensor 800, cockpit sensor 800 being used to collect data for the intelligent cockpit systems of manned aircraft 1000. The intelligent cabin system comprises all vehicle doors, an intelligent seat, a full liquid crystal instrument with a central control screen and an instrument panel integrated, a head lifting display device, a streaming media rearview mirror, a vehicle lamp and the like.
Specifically, the cabin sensor 800 may collect door status data, vehicle light status data, and/or ground air status data, among others. The cabin sensor 800 includes a plurality of processor modules distributed in the cabin, such as door processors, light status processors, ground and air status processors, etc.
The first circuit board 10 acquires the cabin status data of the manned aircraft 1000 through the fifth communication interface E and transmits the data thereof to the second circuit board 20. Further, the second circuit board 20 processes the data and transmits the processed data to the corresponding display device 200. The fifth communication interface E comprises an extended GPIO interface such as a 15-port GPIO interface.
The cockpit status data comprises door status data, lamp status data and/or ground air status data, the first circuit board 10 comprises a fifth communication interface E to connect with the cockpit sensor 800 of the manned aircraft 1000, and the first circuit board 10 acquires the cockpit status data of the manned aircraft 1000 through the fifth communication interface E.
It should be noted that the cabin status data of the manned aircraft is huge, and the data content is only described as an example. The purpose of this application is to demonstrate that the present application can collect and classify cockpit status data for a manned aircraft 1000 via controller 100. The cabin status data of the manned aircraft are used to describe the data. Simple increases and decreases based on this range can be considered as simple alternatives to the present application.
In some embodiments, the predetermined categories further include alarm information, and the second circuit board 20 is further configured to parse the data to generate the alarm information if there is an anomaly in the data.
It can be understood that, abnormal conditions may exist in each system of the manned vehicle 1000, and some abnormal conditions may be directly obtained from connected modules, such as a power module, and when the power obtained by the second circuit board 20 through the fourth communication interface D is reduced to a threshold value, an alarm message may be generated and sent to the display device 200 for warning.
In some embodiments, some abnormal situations require fusion analysis, and the second circuit board 20 of the present application may send the collected data to an extended processor for subsequent processing.
In some embodiments, the controller 100 may control the display device 200 to display the display information of the corresponding category in a predetermined region. The display interface of the display device 200 includes a plurality of display areas, and the second circuit board 20 may be configured to classify data to obtain a plurality of data classifications, where each display area corresponds to one data classification, so that the data is displayed in the corresponding display area.
Accordingly, the contents to be displayed by each display apparatus 200 are not identical, and the required data is classified according to the connected display apparatus 200 and transmitted to the display apparatus 200. It is understood that the display device 200 displays in regions according to a display screen human machine interface design. The second circuit board 20 processes and classifies all the collected data transmitted by the first circuit board 10 according to the display function partition.
Specifically, the display content can comprise a communication signal area, a cabin state area, a flight speed area, a navigation direction, a lifting speed area, an air pressure altitude area, a navigation map area, an electric quantity area, a temperature area, a time area and an alarm area.
For example, referring to FIG. 9, the display of the driving display screen is shown, currently in flight mode. The communication signal area can display effective GPS satellite signals such as 18, data radio station signal intensity, and communication modules which are connected at present such as 5GHz and 2.4GHz, and can display the effective GPS satellite signals in a digital and/or icon mode. The alarm area may display alarm information such as "warning 1: low battery "may be displayed as a number and/or as an icon. The cockpit state area can display the opening and closing states of all the hatches, the car light signs, the names of the current display screens such as driving and the ground and air states such as air, and can display the states in a digital and/or icon mode and the like. The flight speed area displays the instantaneous flight speed of the current manned vehicle and can be dynamically changed. If the mode is the land mode, the current display is the 'running speed', the data is the instantaneous running speed of the current manned aircraft, and the data can be displayed in a digital and/or pointer mode and the like. The navigation direction guide displays the current navigation direction, turning direction and the like of the manned aircraft, and can display in a compass display mode. The lifting speed area comprises the lifting or lowering speed of the current manned vehicle relative to the previous moment, such as 5m/s, and can be displayed in a numerical and/or pointer mode. The barometric altitude area includes the relative altitude, the absolute altitude and a standard barometric altitude of the current manned vehicle, such as 25m, which can be displayed by numbers and/or pointers. The navigation map area comprises map information of the current manned aircraft in a certain range, a navigation route of the manned aircraft, the current position of the manned aircraft in the map and the like. The electric quantity area comprises the display of various electric quantities such as power electric quantity, flight control electric quantity and the like, and can display in the modes of numbers, electric quantity proportion graphs and the like. The temperature area comprises power battery temperature, electric control temperature, motor temperature and the like, and can be displayed in a temperature number mode, a graph mode or the like. The time zone may include time-related information such as the current time of day, the time of flight, etc.
It should be noted that the display device 200 of the present application can display data in a classified manner, and the present embodiment gives a partial display area type. It is to be understood that the above listing of the contents of each region is merely an example to illustrate the functional scope of the region. In some embodiments, the contents of some display areas may be changed, for example, the temperature area may also include the temperature of the manned aircraft body, wing, or other module. Therefore, in the present application, each display area is provided with a function range, and the addition, the subtraction, and the replacement within the function range of the content in each area can be regarded as a simple replacement of the present application.
In this way, the collected data is classified so that the classified data is sent to each corresponding display device for regional display. Different display devices 200 may be enabled to display corresponding real-time dynamic data. The data are classified uniformly, so that the communication transmission work among the modules can be reduced to a certain extent, and the coupling degree among the modules is reduced. Meanwhile, the coupling degree between the display device 200 and each module can be reduced, so that a user can freely add or reduce the display device, and the user experience is enhanced.
Referring to fig. 10, in some embodiments, the controller 100 may be connected to a plurality of or all of the modules. The manned vehicle 1000 includes a flight control system 300, and the first circuit board 10 in the controller 100 is connected to the flight control system 300 via a first communication interface a. The manned vehicle 1000 also includes a plurality of communication modules 400, 410, 420, etc., to which the first circuit board 10 in the controller 100 is connected via a first communication interface B. Manned vehicle 1000 still includes electrical machine module 500 and electricity accent module 600. The first circuit board 10 includes a third communication interface C to connect with the electric motor module 500 and the electric tilt module 600 of the manned aircraft 1000. The manned aircraft 1000 also includes a power module 700. The first circuit board 10 comprises a fourth communication interface D for connection with a power module 700 of the manned aircraft 1000. The manned vehicle 1000 also includes a cockpit sensor 800. The first circuit board 10 comprises a fifth communication interface E for connection with the cabin sensors 800 of the manned aircraft 1000.
Further, the first circuit board 10 collects data and transmits the data to the second circuit board 20, and the second circuit board 20 processes the data and transmits the processed data to the display device 200 for classified display.
To sum up, in the embodiment of the present application, by acquiring part or all of the data of the manned vehicle 1000 in a centralized manner, the data can be managed in a unified manner, and the communication transmission work between the modules is reduced to a certain extent, so that the coupling degree between the modules is reduced. And classifies the data according to a predetermined category and generates corresponding display information, and controls the display device 200 of the manned aircraft 1000 to display the display information of the corresponding classification in a predetermined area. Because the manned aircraft has the characteristic of multiple display devices, different seats need to display different contents. The data is classified into a uniform classification according to predetermined categories and into different classifications according to different display screens, so that each display apparatus 200 can display the display information classified correspondingly in a predetermined area. The coupling degree between the display device 200 and each module can be reduced to a certain extent, and users can freely add or reduce the display devices, thereby enhancing the user experience. And manned vehicle is higher to the demand of safety class data, and safety class data need a plurality of modules to carry out unified processing, and this application can make the safe data acquisition and the categorised back of a plurality of modules, can further send the treater of extension to carry out data analysis and return again. The centralized collection and classification processing of the data can enable the subsequent expanded service to be better realized. Furthermore, the functions of acquisition input, processing and display output are respectively realized by using processors such as different circuit boards or chips, and the like, so that the processing performance of the controller can be effectively improved for the manned aircraft with huge data. In some embodiments, the second circuit board 20 may be connected to a processor by expansion, and send data that requires complex processing such as fusion to the processor, and send data returned by the processor to the display device 200 for corresponding display, so that the controller 100 has good expandability.
The above disclosure provides embodiments or examples to implement the working process of the present application. They are to be considered merely as examples and are not intended to limit the present application. Further, the present application may repeat reference numerals and/or reference letters in the various examples for simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or arrangements discussed. Furthermore, one of ordinary skill in the art will appreciate that: numerous changes, modifications, substitutions and variations can be made to the embodiments without departing from the principles and spirit of the application, the scope of which is defined by the claims and their equivalents.
Claims (13)
1. A controller for a manned aircraft, the manned aircraft further comprising a display device connected to the controller, the controller being configured to:
acquiring data of the manned aircraft;
classifying the data according to a preset category and generating corresponding display information;
controlling the display device to display the display information of the corresponding classification in a preset area;
the controller comprises a first circuit board and a second circuit board electrically connected with the first circuit board, the first circuit board is used for acquiring the data and transmitting the data to the second circuit board, the second circuit board is used for classifying the data according to preset categories and generating corresponding display information, and is used for controlling the display device to display the corresponding classified display information in a preset area, wherein the preset categories comprise attitude data, state data, signal data, cabin state data and/or navigation map data.
2. The controller according to claim 1, wherein the controller is further configured to control the predetermined area of the display device to display the correspondingly classified display information in a predetermined display style.
3. The controller of claim 1, wherein the manned vehicle includes a flight control system configured to collect attitude data of the manned vehicle, the first circuit board includes a first communication interface to communicatively couple with the flight control system, the first circuit board obtains the attitude data via the first communication interface, wherein the attitude data includes roll and/or pitch angles of the manned vehicle.
4. The controller of claim 3, wherein the first circuit board comprises a second communication interface to connect with a plurality of communication modules of the manned vehicle, the first circuit board obtains signal data of the manned vehicle collected by the plurality of communication modules through the second communication interface, and the signal data comprises communication signal data of a plurality of wireless communication signals and/or data transmission stations;
the signal data further comprises GPS data of the manned aircraft, the flight control system is further used for collecting the GPS data, and the first circuit board acquires the GPS data through the first communication interface.
5. The controller of claim 3, wherein said status data comprises speed status data, altitude status data, temperature data, and/or power status data of said manned vehicle, said flight control system further configured to collect status data of said manned vehicle, said first circuit board obtaining said status data via said first communication interface, said status data comprising speed status data and/or altitude status data of said manned vehicle, wherein said speed status data comprises a lift speed and/or a flight speed, and said altitude status data comprises a barometric altitude and/or a radar altitude;
the first circuit board comprises a third communication interface so as to be connected with a motor module and an electric regulation module of the manned aircraft;
the first circuit board comprises a fourth communication interface to be connected with a power module of the manned aircraft, the first circuit board acquires power battery electric quantity data of the power module through the third communication interface and the fourth communication interface to determine the power state data, the power state data further comprises electric quantity data of a flight control system, and the first circuit board acquires the electric quantity data of the flight control system through the first communication interface;
the first circuit board acquires temperature data of the motor module and the electric regulation module through the third communication interface and the fourth communication interface.
6. The controller of claim 3, wherein the navigation map data comprises longitude and latitude data of the manned vehicle, the flight control system is further configured to collect the longitude and latitude data of the manned vehicle, and the first circuit board obtains the longitude and latitude data through the first communication interface to obtain the navigation map data.
7. The controller of claim 6, wherein the navigation map data further comprises map data, and the second circuit board is further configured to fuse the longitude and latitude data with the map data for display by the display device.
8. The controller of claim 1, wherein said cabin status data comprises door status data, light status data and/or ground air status data, and wherein said first circuit board comprises a fifth communication interface for interfacing with a cabin sensor of said manned aircraft, said first circuit board obtaining said cabin status data of said manned aircraft via said fifth communication interface.
9. The controller of claim 1, wherein the predetermined category further comprises alarm information, and wherein the second circuit board is further configured to parse the data to generate the alarm information if there is an anomaly in the data.
10. A control method for a manned aircraft, wherein the controller of any one of claims 1 to 9 is configured to perform the control method, the control method comprising:
acquiring data of the manned aircraft;
classifying the data according to a preset category and generating corresponding display information;
and controlling a display device of the manned aircraft to display the display information of the corresponding classification in a preset area.
11. The control method according to claim 10, wherein the controlling the display device of the manned aircraft to display the display information of the corresponding category in a predetermined area includes:
and controlling the preset area of the display device to display the display information of the corresponding classification in a preset display style.
12. A manned vehicle comprising a controller according to any one of claims 1 to 9.
13. A non-transitory computer-readable storage medium of a computer program, characterized in that, when the computer program is executed by one or more processors, the control method of claim 10 or 11 is implemented.
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