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UAV maximum inclination control method

A control method, the technology of maximum inclination, applied in attitude control, non-electric variable control, control/adjustment system and other directions, can solve problems such as crash, loss, UAV flipping, etc., to achieve accurate flight, solve the effect of flipping

Inactive Publication Date: 2017-05-10
XUZHOU FLY DREAM ELECTRONICS & TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Most of the existing drones are controlled by the remote control. During the flight of the drone, due to improper operation or unfamiliar terrain, the drone will turn over or crash, causing certain losses.

Method used

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Embodiment Construction

[0010] The present invention will be further described below in conjunction with the accompanying drawings.

[0011] Such as image 3 , taking the quadrotor unmanned aerial vehicle as an example, the present invention will be further described.

[0012] A protection device for the maximum inclination angle of an unmanned aerial vehicle is characterized in that it includes a power supply device and a control device.

[0013] Further, the UAV is a multi-rotor UAV.

[0014] Further, the power supply device is a battery.

[0015] Further, the control device includes an electronic speed controller, a receiver and a driving motor.

[0016] Further, the electronic governor is a brushless electronic governor.

[0017] Further, the electronic governor and the driving motor are installed on each rotor of the drone, and the electronic governor is installed under the driving motor.

[0018] The control device includes an electronic governor, an autopilot and a drive motor.

[0019] ...

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PUM

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Abstract

The invention discloses a UAV maximum inclination control method The method includes that when the UAV flight inclination angle is greater than the set value m, the control signal is transmitted to an electronic governor through a receiver, the electronic governor controls a servomotor, and the operating speed of the servomotor is reduced, and when the flight state of the UVA recovers to the horizontal state, the electronic governor control the servomotor to accelerate the operation, and the UAV continues to fly. According to the method, the problems of overturn, course deviation, and out-of-control crash of the UVA in the flight process are solved, and accurate flight can be achieved.

Description

technical field [0001] The invention relates to a method for controlling the maximum inclination angle of an unmanned aerial vehicle. Background technique [0002] With the rapid rise of the aircraft model industry, especially multi-rotor UAVs have been more and more widely used. For example, it plays an important role in agricultural plant protection, urban aerial photography, meteorological analysis, power inspection and other fields. Most of the existing drones are controlled by remote control. During the flight of the drone, due to improper operation or unfamiliar terrain, the drone will flip or crash, causing certain losses. Contents of the invention [0003] Aiming at the shortcomings of the above-mentioned technologies, the present invention provides a method for controlling the maximum inclination angle of the UAV, which solves the problem that the UAV overturns and crashes or is damaged due to excessive braking speed during flight. [0004] A method for controll...

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 阚森
Owner XUZHOU FLY DREAM ELECTRONICS & TECH
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