CN215475779U - A controller and manned vehicle for manned vehicle - Google Patents

Abstract

The application discloses controller for manned vehicle, manned vehicle still include the display device who is connected with the controller, the controller include first circuit board and with first circuit board electric connection's second circuit board, first circuit board is used for acquireing manned vehicle's data to with data transmission to second circuit board, the second circuit board is used for handling data and generates display information, in order to show display information through display device. Therefore, dynamic data and static data generated by the manned aircraft in various working modes can be collected and processed, and each display device can further display the required data. The application also discloses a manned aircraft.

Description

A controller and manned vehicle for manned vehicle

Technical Field

The application relates to the technical field of manned aircrafts, in particular to a controller for the manned aircrafts and the manned aircrafts.

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 carry out effective operation in time. How to effectively provide data of manned aircrafts for drivers and passengers becomes an urgent problem to be solved.

SUMMERY OF THE UTILITY MODEL

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 purpose of the application is to provide a controller and a manned aircraft.

The embodiment of the application provides a controller for manned vehicle, manned vehicle still include with the display device that the controller is connected, the controller include first circuit board and with first circuit board electric connection's second circuit board, first circuit board is used for acquireing manned vehicle's data, and will data transmission extremely the second circuit board, the second circuit board is used for handling data generation display information, in order to pass through display device shows display information.

In some embodiments, the manned vehicle includes a flight control system for collecting attitude data, state data, longitude and latitude data of a navigation map, electrical data of a flight control system, and/or GPS data of the manned vehicle, the first circuit board comprises a first communication interface to be in communication connection with the flight control system, the first circuit board acquires data collected by the flight control system through the first communication interface, wherein the attitude data comprises roll and/or pitch angles of the manned aerial vehicle, said status data comprising speed status data and/or altitude status data of said manned vehicle, 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.

In some embodiments, the first circuit board is further configured to obtain abnormal data information sent by the flight control system through the first communication interface, so that the second circuit board may generate alarm information according to the abnormal data information.

In some embodiments, the first circuit board includes a second communication interface to connect with a plurality of communication modules of the manned aircraft, the first circuit board obtains signal data of the manned aircraft collected by the plurality of communication modules through the first communication interface, the signal data includes communication signal data of a plurality of wireless communication signals and/or data transmission stations, and the second circuit board is configured to parse the signal data to generate warning information when the signal data is abnormal.

In some embodiments, the first circuit board includes a third communication interface to connect with an electric motor module and an electric tilt module of the manned aircraft, the first circuit board obtains temperature data of the electric motor module and the electric tilt module through the third communication interface, and the second circuit board is configured to parse the temperature data to generate warning information when the temperature data is abnormal.

In some embodiments, the first circuit board includes a fourth communication interface to connect with a power module of the manned aircraft, the first circuit board obtains electric quantity data of the power module through the fourth communication interface to determine flight power parameters of the manned aircraft, and the second circuit board is configured to analyze the flight power parameters to generate warning information when the flight power parameters are abnormal.

In some embodiments, the first circuit board comprises a fifth communication interface for connecting with a cabin sensor of the manned aircraft, the first circuit board obtains cabin status data of the manned aircraft through the fifth communication interface, the cabin status data comprises door status data, vehicle light status data and/or ground air status data, and the second circuit board is used for analyzing the cabin status data to generate warning information when the cabin status data is abnormal.

In some embodiments, the display device includes a plurality of display areas, and the second circuit board is configured to classify the data to obtain a plurality of classification data, each of the display areas corresponds to one of the classification data, so that the data is displayed in the corresponding display area.

In some embodiments, the display devices include a plurality of display devices, the second circuit board is electrically connected to the plurality of display devices, respectively, and the second circuit board is configured to process the data to generate display information and distribute the display information to a predetermined display device for display according to the content of the display information.

The application also provides a manned aircraft, which comprises the controller.

The controller for the manned aircraft comprises a first circuit board and a second circuit board electrically connected with the first circuit board. The data of the manned aircraft are acquired by the first circuit board, the data are transmitted to the second circuit board, and meanwhile the second circuit board is used for processing the data to generate display information, so that the generated display information is displayed through the display device. Therefore, dynamic data and static data generated by the manned aircraft in various working modes can be collected and processed, and each display device can further display the required data. 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 respectively of multimode among the prior art, this application unifies data acquisition to first circuit board, can unify the management to data, reduces the communication transmission work between each module to a certain extent to reduce the coupling degree between each module.

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 structural diagram of a controller 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 structural diagram of a controller 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 diagram showing an example of an interface of a display device according to an embodiment of the present application;

fig. 9 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 or similar reference numerals refer to the same or similar elements or elements having the same or similar function throughout. The embodiments described below with reference to the accompanying drawings are illustrative and are only for the purpose of 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, the present embodiment provides a controller 100 for a manned vehicle, the manned vehicle includes a display device 200 connected to the controller 100, the controller 100 includes a first circuit board 10 and a second circuit board 20 electrically connected to the first circuit board, the first circuit board 10 is configured to acquire data of the manned vehicle and transmit the data to the second circuit board 20, and the second circuit board 20 is configured to process the data to generate display information, so that the generated display information is displayed by the display device 200.

Referring to fig. 2, the present embodiment further provides a manned vehicle 1000, and the manned vehicle 1000 includes the controller 100 and the display device 200 of the present embodiment.

As an emerging vehicle, the related technology of the manned vehicle is rapidly developing and perfecting, and the manned vehicle comprises an aerocar, 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 obtain partial data such as flight status data, security data, etc. in real time. And the required data or state is displayed in real time through equipment such as a display screen.

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. 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, and their positional relationship includes separate circuit boards or integration.

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 data of the manned aircraft can comprise data, state data, motor data, electric control data, alarm data and the like during flight. The system can also comprise dynamic data and static data of the manned vehicle in various working modes, including partial data or all data. The acquisition mode comprises real-time active acquisition or active input of external equipment, and the specific mode is set according to data and equipment types. 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 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 current real-time electric quantity of the first circuit board 10 can be further calculated.

When the first circuit board 10 acquires data of the manned vehicle 1000, the data is transmitted to the second circuit board 20. After receiving the data, the second circuit board 20 performs corresponding processing and generates data for displaying information. Processing includes, but is not limited to, basic data screening, deduplication, and classification, among others. 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.

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.

Further, the preprocessed data are classified based on 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 predetermined categories of electric quantities. Or classifying based on function, for example, classifying all data collected from the flight control system into a predetermined category of the flight control system if the flight control system functions.

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 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 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 data processing is completed, the second circuit board 20 generates display information, and then sends the display information to the display device 200 for displaying. 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 manner, the controller 100 for the manned vehicle 1000 of the present application generates display information by acquiring data of the manned vehicle using the first circuit board 10 and transmitting the data to the second circuit board 20, while processing the data using the second circuit board 20 to display the generated display information through the display device 200. So that the dynamic data and the static data generated by the manned vehicle 1000 in various working modes can be collected and processed, such as classified, and the display devices 200 can display the required data. 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 multiple modules in the prior art, data collection is unified to the first circuit board 10, data can be managed in a unified mode, communication transmission work among the modules is reduced to a certain extent, and therefore coupling degree among the modules is reduced.

Referring to FIG. 3, in some embodiments, manned aircraft 1000 also includes flight control system 300. The flight control system 300 is mainly used to ensure the stability and maneuverability of the manned vehicle 1000, enhance the safety of flight, and reduce the burden on the pilot. Including aircraft pitch, roll and yaw control, high lift and high drag control, manual trim, direct force control, and other configuration-changing controls for aircraft such as changing wing sweep, horizontal stabilizer stagger, etc.

The flight control system 300 may be used to collect attitude data, status data, longitude and latitude data of a manned vehicle, electrical data of the flight control system, and/or GPS data. Wherein the attitude data of the manned vehicle includes roll and/or pitch angles of the manned vehicle 1000. The manned vehicle status data includes speed status data and/or altitude status data for the manned vehicle 1000, wherein the speed status data includes lift speed and/or flight speed and the altitude status data includes barometric altitude and/or radar altitude. The longitude and latitude data of the navigation map is the current coordinate position information of the manned vehicle 1000, and provides data display for the navigation system of the manned vehicle together with the map display of the manned vehicle.

Further, the first circuit board 10 includes a first communication interface a, the first communication interface a includes a plurality of 232 interfaces, and 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 obtain the data collected by the flight control system 300 through the first communication interface a.

In some embodiments, the first circuit board 10 may be configured to obtain the abnormal data information sent by the flight control system 300 through the first communication interface a so that the second circuit board 20 may generate the warning information according to the abnormal data information.

Specifically, the first circuit board 10 may receive the warning information transmitted by the flight control system 300 through the first communication interface a, and thereby transmit the warning information to the second circuit board 20. The second circuit board 20 may also process the data information of the flight control system 300 transmitted by the first circuit board 10 to generate warning information and transmit the warning information to the display device 200 for displaying a warning. For example, the flight control system 300 acquires the flight control battery power and the current speed of the manned vehicle, calculates the speed power by the second circuit board 20 to obtain that the flight control battery power is lower than the threshold value, and generates the warning information to be sent to the corresponding display device 200.

Referring to FIG. 4, in some embodiments, manned aircraft 1000 also includes a plurality of communication modules 400, 410, 420, etc. The first circuit board 10 comprises a second communication interface B by means of which the first circuit board 10 can be connected with a plurality of communication modules 400, 410, 420, etc. of the manned aircraft.

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. Meanwhile, the manned vehicle 1000 is used to acquire wireless communication data such as audio and video, images, text and other information in real time. 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 aircraft 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 second circuit board 20 may be configured to process the signal data to generate display information to be transmitted to the plurality of display devices 200, and/or to parse the signal data to generate alarm information when there is an abnormality in the signal data.

Referring to fig. 5, in some embodiments, manned aircraft 1000 further includes a motor module 500 and an electrical tilt module 600. The first circuit board 10 includes a third communication interface C, and the first circuit board 10 may be connected to the electric motor module 500 and the electric tilt module 600 of the manned aircraft 1000 through the third communication interface C.

The third communication interface C includes CAN interfaces, which may include CAN1, CAN2, and the like 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 first circuit board 10 may obtain temperature data of the motor module 500 and the electrical tilt module 600 through the third communication interface C, and send the temperature data to the second circuit board 20, and the second circuit board 20 processes the temperature data and sends the data to the corresponding display device 200. Meanwhile, the temperature data can be analyzed to generate alarm information when the temperature data is abnormal.

Referring to FIG. 6, in some embodiments, manned aircraft 1000 also includes a power module 700. The first circuit board 10 comprises a fourth communication interface D, through which the first circuit board 10 is connected with the power module 700 of the manned aircraft 1000. The first circuit board 10 can acquire the electric quantity data of the power module 700 through the fourth communication interface D to determine the flight power parameters of the manned vehicle 1000. 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 flight power parameters comprise electric quantity data, electric control temperature data and motor temperature data of different batteries. The first circuit board 10 can obtain the electric control temperature data and the motor temperature data through the third communication interface C and the fourth communication interface D.

Meanwhile, the second circuit board 20 may also be used to analyze the flight power parameter to generate an alarm message when there is an abnormality in the flight power parameter.

Referring to FIG. 7, in some embodiments, manned aircraft 1000 also includes cockpit sensor 800. The first circuit board 10 comprises a fifth communication interface E, via which the first circuit board 10 is connected to the cockpit sensors 800 of the manned aircraft 1000. The cockpit sensor 800 may collect cockpit status data of the manned vehicle 1000, including door status data, lamp status data, and/or ground air status data, etc. The cabin sensor 800 is used for acquiring vehicle door state data, vehicle lamp state data and/or ground air state data, and comprises a plurality of processor modules dispersed in a cabin. Such as various door processors, vehicle light status processors, ground air status processors, etc.

The first circuit board 10 acquires the cabin state data of the manned aircraft 1000 through the fifth communication interface E and transmits the data to the second circuit board 20, and the second circuit board 20 processes the data and transmits the data to the corresponding display device 200. The fifth communication interface E comprises an extended GPIO interface such as a 15-port GPIO interface.

Meanwhile, the second circuit board 20 may also be used to parse the cabin status data to generate warning information when there is an anomaly in the cabin status data.

In some embodiments, 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, each display area corresponding to one data classification, so that the data is displayed in the corresponding display area.

Specifically, the second circuit board 20 may classify the data collected and transmitted by the first circuit board 10. The classification may be based on the display interface requirements of the connected display device 200. Further, the display interface generally divides the display content according to the display area. Such as a speed region showing the speed of travel of the current manned vehicle 1000.

Accordingly, the contents to be displayed by each display apparatus 200 are not exactly the same, 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.

In some embodiments, the present application may divide the display content into a communication signal area, a cabin status area, a flight speed area, a navigation direction, a lifting speed area, a barometric altitude area, a navigation map area, a power area, a temperature area, a time area, and an alarm area.

For example, referring to FIG. 8, 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: too low a power level "may be displayed numerically and/or graphically. 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 includes the speed of the current manned vehicle rising or falling 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 the 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 display of various electric quantities such as power electric quantity, flight control electric quantity and the like, and can display in a digital mode, an electric quantity proportion digital mode or an electric quantity proportion graph mode 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 classify display data, and the present embodiment gives a kind of partial display area. 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, wings, etc. 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 area display. Different display devices 200 may be enabled to display corresponding real-time dynamic data. The data are classified uniformly, and the communication transmission work among the modules can be reduced to a certain extent, so that 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.

In some embodiments, the display device 200 includes a plurality of display devices 200, the second circuit board 20 is electrically connected to the plurality of display devices 200, and the second circuit board 20 is configured to process data to generate display information and distribute the display information to a predetermined display device for displaying according to the content of the display information.

Referring to fig. 9, 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 also includes motor module 500 and electrically tunable module 600. The first circuit board 10 includes a third communication interface C to connect with the motor module 500 and the electric tilt module 600 of the manned aircraft 1000. The manned vehicle 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 vehicle 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.

In summary, the controller 100 for the manned vehicle 1000 according to the present application acquires data of the manned vehicle by using the first circuit board 10, transmits the data to the second circuit board 20, and simultaneously processes the data by using the second circuit board 20 to generate display information, so as to display the generated display information through the display device 200. So that the dynamic data and static data generated by the manned vehicle 1000 in various working modes can be collected and processed, such as classified, and each display device 200 can display the required data. Meanwhile, as the manned aircraft has huge data volume, the functions of acquisition input, processing and display output are respectively realized by using processors such as different circuit boards or chips, and the processing performance of the controller can be effectively improved. Further, for collection of multiple modules in the prior art, data collection is unified to the first circuit board 10, data can be managed in a unified mode, communication transmission work among the modules is reduced to a certain extent, and therefore coupling degree among the modules is reduced. In the data processing, the collected data is classified, so that the classified data is sent to each corresponding display device for area display. Different display devices 200 may be enabled to display corresponding real-time dynamic data. The data are classified uniformly, and the communication transmission work among the modules can be reduced to a certain extent, so that 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. In some embodiments, the second circuit board 20 may be connected to a processor in an expansion manner, 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. Moreover, the present application may repeat reference numerals and/or letters in the various examples, such repetition is for the purpose of simplicity and clarity and does not in itself dictate a relationship between the various embodiments and/or configurations discussed. Further, one of ordinary skill in the art will appreciate that: numerous changes, modifications, substitutions and alterations 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 (10)

1. The utility model provides a controller for manned vehicle, its characterized in that, manned vehicle still include with display device that the controller is connected, the controller include first circuit board and with first circuit board electric connection's second circuit board, first circuit board be used for acquireing manned vehicle's data, and will data transmission extremely the second circuit board, the second circuit board is used for handling data generation display information, with through display device shows display information.

2. The controller of claim 1, wherein the manned vehicle includes a flight control system, the flight control system is used for collecting attitude data and state data of the manned aircraft, longitude and latitude data of a navigation map, electric quantity data and/or GPS data of the flight control system, the first circuit board comprises a first communication interface to be in communication connection with the flight control system, the first circuit board acquires data collected by the flight control system through the first communication interface, wherein the attitude data comprises roll and/or pitch angles of the manned aerial vehicle, said status data comprising speed status data and/or altitude status data of said manned vehicle, 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.

3. The controller of claim 2, wherein the first circuit board is further configured to obtain abnormal data information sent by the flight control system through the first communication interface, so that the second circuit board can generate alarm information according to the abnormal data information.

4. The controller according to claim 1, 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, the signal data comprises communication signal data of a plurality of wireless communication signals and/or data transmission stations, and the second circuit board is used for analyzing the signal data to generate alarm information when the signal data is abnormal.

5. The controller according to claim 1, wherein the first circuit board comprises a third communication interface to connect with an electric motor module and an electric tilt module of the manned aircraft, the first circuit board obtains temperature data of the electric motor module and the electric tilt module through the third communication interface, and the second circuit board is configured to parse the temperature data to generate alarm information when the temperature data is abnormal.

6. The controller according to claim 1, wherein the first circuit board comprises a fourth communication interface for connecting with a power module of the manned vehicle, the first circuit board obtains power data of the power module through the fourth communication interface to determine flight power parameters of the manned vehicle, and the second circuit board is configured to analyze the flight power parameters to generate warning information when the flight power parameters are abnormal.

7. The controller of claim 1, wherein the first circuit board comprises a fifth communication interface for connecting with a cockpit sensor of the manned vehicle, the first circuit board obtains cockpit status data of the manned vehicle through the fifth communication interface, the cockpit status data comprises door status data, vehicle light status data and/or ground air status data, and the second circuit board is configured to parse the cockpit status data to generate warning information when there is an anomaly in the cockpit status data.

8. The controller according to any one of claims 1-7, wherein the display device comprises a plurality of display areas, the second circuit board is configured to classify the data to obtain a plurality of classified data, and each display area corresponds to one of the classified data, so that the data is displayed in the corresponding display area.

9. The controller according to any one of claims 1 to 7, wherein the display device includes a plurality of display devices, the second circuit board is electrically connected to the plurality of display devices, respectively, and the second circuit board is configured to process the data to generate display information and distribute the display information to a predetermined display device for display according to the content of the display information.

10. A manned vehicle comprising a controller according to any one of claims 1 to 9.

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