Unmanned aerial vehicle control system

A technology of unmanned aerial vehicles and control systems, which is applied in the field of unmanned aerial vehicle control systems, can solve problems such as the inability to automatically control, and achieve the effects of simple and reliable structure, convenient operation, and light weight

Active Publication Date: 2016-01-27
XIANGYANG HONGWEI AIRCRAFT
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] In view of the above defects or improvement needs of the prior art, the object of the present invention is to provide a control system for unmanned aerial vehicles, wherein by improving its key control system composition, the connection relationship between components, etc., compared with the prior art It can effectively solve the problem that the existing aircraft contro

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  • Unmanned aerial vehicle control system

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Embodiment 1

[0024] Such as figure 1 As shown, the UAV intelligent control system in the present invention mainly includes a flight controller 1, an UAV 2, a power supply module 3, a left and right wing control device 4, a throttle throttle control device 5, a start and stop circuit 6, and a task system 7 , flameout protection circuit 8, GPS navigation system 9, height measuring device 10, three-dimensional imaging device 11, obstacle avoidance sensor 12 and ground station 13.

[0025] The flight controller 1 is installed and fixed on the unmanned aerial vehicle 2, and can control all command actions of the unmanned aerial vehicle 2 from starting flight to flame-out and landing; The unmanned aerial vehicle 2 supplies power; the left and right wing control devices 4 are connected with the flight controller 1 through lines, and control the takeoff, landing, left turn and right turn attitude of the unmanned aerial vehicle 2 by the instructions of the flight controller 1; The input end of the...

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Abstract

The invention discloses an unmanned aerial vehicle control system comprising a flight controller and a flame-out protection line. The flame-out protection line is directly connected with the engine of an unmanned aerial vehicle and used for limiting starting of the engine of the unmanned aerial vehicle. The flight controller is installed on the unmanned aerial vehicle and used for controlling the unmanned aerial vehicle. The flight controller is connected with the unmanned aerial vehicle via a left and right wing control device, an air door and throttle control device and a start and flame-out line and used for controlling the engine of the unmanned aerial vehicle and the flight attitude of the unmanned aerial vehicle. Take-off, landing and flight speed of the unmanned aerial vehicle can be intelligently controlled, and the unmanned aerial vehicle control system can also record the operation process of the unmanned aerial vehicle in real time and monitor obstacles on the way apart from the given tasks so that the unmanned aerial vehicle control system has great effect in monitoring and tracing the flight process of the aerial vehicle.

Description

technical field [0001] The invention belongs to the field of control technology and wireless communication, and more specifically relates to a control system of an unmanned aerial vehicle. Background technique [0002] Unmanned aerial vehicles can fly at low altitude and low speed, perform low-altitude mission operations, have good maneuverability and concealment, and cover a wide range of application fields. Existing unmanned aerial vehicles often directly use manual real-time control to operate the attitude of the unmanned aerial vehicle (such as take-off, landing, left turn, right turn, hovering, etc.), which limits the working radius of the unmanned aerial vehicle. [0003] At present, there are more and more types and quantities of commercial or agricultural unmanned aerial vehicles in our country, making the corresponding application operations easier and more convenient. However, the flight control technology of my country's unmanned aerial vehicles is still relative...

Claims

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Application Information

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IPC IPC(8): G05D1/08G05D1/10
Inventor 胡明军薛龙薛富利刘晓军卢文龙雷自力
Owner XIANGYANG HONGWEI AIRCRAFT
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