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Anti-radiation flight controller of unmanned aerial vehicle

A flight controller, anti-radiation technology, applied in the direction of computer control, program control, general control system, etc., can solve the problems of poor anti-interference ability of the controller, crash of the controller, error, etc., to reduce the occurrence of crashes, dismantling Simple and convenient installation, improve the effect of protection performance

Pending Publication Date: 2022-03-01
上海忆伯科技股份有限公司
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  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] At present, the existing unmanned aerial vehicle attitude control system on the market is mainly designed for civilian consumer products. The controller has no anti-radiation shell, no backup redundant circuit design, uses a single-threaded CPU, the CPU has no fault-tolerant computing capability, and the CPU has no radiation. The radiation protection ability of the controller is poor, and the comprehensive anti-interference ability of the controller is poor. The stability of the aircraft using this type of controller is not high in the radiation area. The accident rate of man-machine crashes has increased sharply, and it cannot be used for flight reconnaissance and detection missions in radiation areas

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  • Anti-radiation flight controller of unmanned aerial vehicle
  • Anti-radiation flight controller of unmanned aerial vehicle
  • Anti-radiation flight controller of unmanned aerial vehicle

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Embodiment Construction

[0048] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some, not all, embodiments of the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0049] In describing the present invention, it is to be understood that the terms "opening", "upper", "lower", "thickness", "top", "middle", "length", "inner", "surrounding" etc. Indicating orientation or positional relationship is only for the convenience of describing the present invention and simplifying the description, and does not indicate or imply that the components or elements referred to must have a specific orientation, be constructed and operated in a sp...

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Abstract

The anti-radiation flight controller comprises a control mechanism and an anti-radiation box installed outside the control mechanism in a matched mode, and the anti-radiation box is sleeved with a heat dissipation box. The anti-radiation box is arranged outside the control mechanism, high reliability can be achieved when an aircraft in an area within a certain irradiation intensity range flies, air crash accidents are reduced, the flight investigation task in the radiation area is completed, the anti-radiation box can be conveniently disassembled from the outside of the control mechanism, disassembly and assembly are easy and convenient, and the anti-radiation box is convenient to use. The method is suitable for practical use; a plurality of processors are arranged, so that data exchange can be performed through respective data buses, and fault-tolerant calculation capability is realized; and the heat dissipation box is arranged outside the anti-radiation box, so that the protection performance is improved.

Description

technical field [0001] The invention belongs to the technical field of flight equipment, in particular to a radiation-resistant flight controller for an unmanned aerial vehicle. Background technique [0002] At present, the existing unmanned aerial vehicle attitude control system on the market is mainly designed for civilian consumer products. The controller has no anti-radiation shell, no backup redundant circuit design, uses a single-threaded CPU, the CPU has no fault-tolerant computing capability, and the CPU has no radiation. The radiation protection ability of the controller is poor, and the comprehensive anti-interference ability of the controller is poor. The stability of the aircraft using this type of controller is not high in the radiation area. The accident rate of man-machine crashes has increased sharply, and it cannot be used for flight reconnaissance and detection missions in radiation areas. Contents of the invention [0003] The purpose of the present inv...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05B19/042
CPCG05B19/0423G05B2219/25257
Inventor 许虎徐伯胜
Owner 上海忆伯科技股份有限公司