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Undisturbed switching method and device for redundant flight control module of unmanned aerial vehicle

A non-disruptive switching and UAV technology, applied in aircraft control, transportation and packaging, aircraft parts, etc., can solve the problems of potential safety hazards and the inability to effectively monitor the status of UAVs, so as to avoid loss and realize non-disruptive switching Effect

Pending Publication Date: 2022-07-12
长春长光博翔无人机有限公司
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  • Abstract
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AI Technical Summary

Problems solved by technology

[0005] However, the inventor found that the main flight controller will only synchronize the flight data when it is in a normal working state. Any flight data, resulting in the inability to effectively monitor the status of the UAV when it restores the main control function, there are certain security risks

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  • Undisturbed switching method and device for redundant flight control module of unmanned aerial vehicle
  • Undisturbed switching method and device for redundant flight control module of unmanned aerial vehicle
  • Undisturbed switching method and device for redundant flight control module of unmanned aerial vehicle

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Embodiment Construction

[0040] In order to make the objectives, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail below with reference to the accompanying drawings and specific embodiments. It should be understood that the specific embodiments described herein are only used to explain the present invention, but not to limit the present invention.

[0041] see figure 1 , is a flow chart of a method for undisturbed switching of a redundant flight control module of an unmanned aerial vehicle according to an embodiment of the present invention. The method is applied to a disturbanceless switching device of a redundant flight control module of an unmanned aerial vehicle. The device includes a first flight control module and the second flight control module;

[0042] The method includes the following steps:

[0043] First, go to step S101 to set the first flight control module as the master control module, the second flight cont...

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Abstract

The invention provides an undisturbed switching method and device for redundant flight control modules of an unmanned aerial vehicle, and the device comprises the steps: enabling a first flight control module and a second flight control module to transmit PWM wave signals with a preset frequency to each other so as to monitor the states of each other, and enabling the other flight control module to be set as a main control module when one flight control module breaks down, since the data is always bidirectionally transmitted between the first flight control module and the second flight control module, the first flight control module can receive the flight data transmitted by the second flight control module at the first time for synchronization after the first flight control module breaks down and then recovers the main control function, thereby realizing the undisturbed switching of the flight control of the unmanned aerial vehicle.

Description

technical field [0001] The invention relates to the field of unmanned aerial vehicle flight control, in particular to a disturbance-free switching method and device of a redundant flight control module of an unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicle, referred to as "UAV", is an unmanned aerial vehicle controlled by radio remote control equipment or its own program control device. With the development of science and technology, UAV technology is becoming more and more mature. UAVs are widely used due to their fast speed, flexible operation, wide application, low cost, and good maneuverability. They not only play an extremely important role in modern warfare. , and has a broader prospect in the civilian field. [0003] The UAV flight control module is the core of the UAV. For UAVs using a single flight control module, if the flight control module is abnormal or faulty during the flight, it will directly cause the UAV flight control to appe...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C19/00
CPCB64C19/00B64U2201/00
Inventor 王东白越裴信彪王帆杨生李会彬
Owner 长春长光博翔无人机有限公司
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