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A fixed wing unmanned aerial vehicle control system

A control system and drone technology, applied in the field of drones, can solve problems such as the inability to guarantee the safety of users, the stability of drone performance, the inability to realize remote control, and the limitation of flight range, so as to achieve stable performance of drones, The effect of safety, stability and diversified functions

Inactive Publication Date: 2018-02-02
成都立威斯科技有限公司
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  • Description
  • Claims
  • Application Information

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Problems solved by technology

However, the flight range of fixed-wing UAVs is limited by the visual distance of the operator and the radio transmission range of the remote control. Therefore, it is necessary to design an automatic control system for fixed-wing UAVs with high-precision trajectory tracking.
[0003] The current fixed-wing drones cannot realize the three control methods of remote control, ground station control, and self-program control; they cannot guarantee the safety of users and the stability of drone performance.

Method used

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  • A fixed wing unmanned aerial vehicle control system

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Embodiment 1

[0025] The present invention is realized through the following technical solutions, as figure 1 As shown, a fixed-wing unmanned aerial vehicle control system is connected with the PC and the remote control respectively, and also includes a data processing module connected with the remote control and the PC respectively, a data acquisition module connected with the data processing module, a steering gear / motor And the mission mechanism; the data acquisition module includes a gyroscope module, an accelerometer module, a magnetometer module, an altimeter module, a GPS module, and an airspeed module that are respectively connected with the data processing module.

[0026] It should be noted that, through the above improvements,

[0027] Other parts of this embodiment are the same as those of the foregoing embodiments, so details are not repeated here.

Embodiment 2

[0029] This embodiment is further optimized on the basis of the above embodiments, such as figure 1 As shown, further, in order to better realize the present invention, the data processing module is provided with a UART communication interface, and the gyroscope module, the accelerometer module, the magnetometer module and the GPS module communicate with the data processing module through the UART communication interface. module connection.

[0030] Further, in order to better realize the present invention, the data module is provided with an A / D conversion interface; the altimeter module and the airspeed module are connected to the data processing module through the A / D conversion interface.

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Abstract

The invention provides a fixed wing unmanned aerial vehicle control system which is connected with a PC and a remote controller. The system comprises a data processing module connected with the remotecontroller and the PC, a data collection module connected with the data processing module, a steering engine / electromotor and a task mechanism. The data collection module comprises a gyroscope module, an accelerometer module, a magnetometer module, an altitude meter module, a GPS module and an airspeedometer module, which are connected with the data processing module. The fixed wing unmanned aerial vehicle control system achieves three control modes, namely remote control, ground station control and self-program control. The system is safe and stable and can guarantee the safety of users andstability of performance of an unmanned aerial vehicle. The system has diversified functions, such as automatic take-off and landing, flight along airlines and task execution according to requirements.

Description

technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular, a control system for fixed-wing unmanned aerial vehicles. Background technique [0002] Fixed-wing UAVs are widely used in enemy reconnaissance, precision strikes, forest fire prevention, surveying and mapping and other fields due to their advantages such as fast flight speed, long battery life, and large load. However, the flight range of fixed-wing UAVs is limited by the visual distance of the operator and the radio transmission range of the remote control. Therefore, it is necessary to design an automatic control system for fixed-wing UAVs with high-precision trajectory tracking. [0003] The current fixed-wing drones cannot realize the three control methods of remote control, ground station control, and self-program control; they cannot guarantee the safety of users and the stability of drone performance. Contents of the invention [0004] The purpose of the...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/08G05D1/10
CPCG05D1/0808G05D1/101
Inventor 姚清群
Owner 成都立威斯科技有限公司
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