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Flight control method and apparatus for multiaxial flight vehicle

A technology for multi-rotor aircraft and flight control, which is applied in the field of flight control methods and devices for multi-rotor aircraft, and can solve problems such as the inability of multi-rotor aircraft to maintain balance and land smoothly.

Active Publication Date: 2016-01-20
SICHUAN AEE AVIATION TECH CO LTD
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AI Technical Summary

Problems solved by technology

[0004] The main purpose of the present invention is to provide a method and device for flight control of a multi-axis aircraft, aiming to solve the problem that the multi-axis aircraft cannot maintain balance and land smoothly when any power system of the multi-axis aircraft is abnormal

Method used

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  • Flight control method and apparatus for multiaxial flight vehicle
  • Flight control method and apparatus for multiaxial flight vehicle
  • Flight control method and apparatus for multiaxial flight vehicle

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no. 1 example

[0060] Reference figure 1 , Is the first embodiment of the flight control method of the multi-axis aircraft of the present invention, and the method includes:

[0061] In step S100, the flight control system detects whether an abnormality occurs in any one of the plurality of power systems designed for axles, and the abnormality includes: complete failure of the power system and incomplete failure of the power system;

[0062] Among them, take a quadcopter as an example for illustration, such as Picture 10 In the quadrocopter shown, power system A and power system C are designed for axis, power system B and power system D are designed for axis, power system A and power system C are for each other, power system B and power system D The axis is mutually aligned, and the flight control system obtains the current state through a plurality of sensors included in the multi-axis aircraft, and judges whether there is any abnormality of the power system of the multi-axis aircraft according ...

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Abstract

The invention discloses a flight control method and apparatus for a multiaxial flight vehicle. The method includes: detecting whether a plurality of power systems with countershaft design are abnormal by a flight control system; and when the flight control system detects that any power system is abnormal, adjusting the countershaft power system to make the multiaxial flight vehicle land stably. The method and the apparatus provided by the invention solve the problem that the multiaxial flight vehicle cannot maintain balance when any power system in the multiaxial flight vehicle is abnormal in the prior art, and the multiaxial flight vehicle still can land stably when abnormality occurs to any power system of the multiaxial flight vehicle.

Description

Technical field [0001] The invention relates to the field of aircraft flight control, in particular to a method and device for flight control of a multi-axis aircraft. Background technique [0002] At present, multi-axis aircraft are widely used in civil, commercial and military fields. In the civilian field, more and more extreme sports enthusiasts use multi-axis aircraft for video recording. In the commercial field, in addition to carrying video equipment for various sports events In addition to tracking aerial photography, it has entered the logistics industry and can send goods to remote areas where human distribution is difficult and slow. Therefore, multi-axis aircraft has a wide range of applications and broad market prospects. [0003] The existing multi-axis aircraft uses a multi-axis power system to provide power and maintain balance. Therefore, after any power system is abnormal, the multi-axis power system will lose balance and crash, causing damage to the aircraft and ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C39/02G05D1/10G05D1/08
Inventor 张显志
Owner SICHUAN AEE AVIATION TECH CO LTD
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