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Flight control debugging protecting device of multi-rotor-wing unmanned plane

A multi-rotor unmanned aerial vehicle and protection device technology, applied in the aviation field, can solve problems such as easy damage, aircraft falling damage, economic loss of participants, etc., to ensure safety, avoid research risks, and avoid property losses.

Inactive Publication Date: 2015-07-22
NORTHWEST A & F UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in stark contrast, in the field of practical application, the development of new flight control algorithms is not rapid, and the transformation of scientific research results is very slow
After a large number of theoretically very advanced algorithms were proposed, they could not be put into practical application because of their immaturity and instability. Many excellent ideas were shelved after they were proposed, and could not be further tested and improved. Therefore, the work cannot be carried out
The reason is that drones are expensive and easily damaged equipment. Many advanced flight control algorithms are low in completion and poor in stability. Cause the participants of the related research to suffer greater economic loss
However, a new flight control algorithm needs to be repeatedly debugged from its proposal to its perfection. Researchers will have to take the risk of suffering heavy losses and carry out a large number of test flights before they can complete the work. The risk of research is very high.
This has objectively greatly increased the research and development cost of new flight control algorithms in the application field, and directly affected the speed at which new theories are transformed into new achievements.

Method used

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  • Flight control debugging protecting device of multi-rotor-wing unmanned plane
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  • Flight control debugging protecting device of multi-rotor-wing unmanned plane

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Embodiment Construction

[0023] The present invention is further described below in conjunction with accompanying drawing:

[0024] The present invention aims at the independent debugging of the three degrees of freedom of roll, pitch and heading and the comprehensive debugging of the three degrees of freedom for the flight control system of the multi-rotor UAV; the overall effect and the coordinate system of the UAV carrier are as follows: figure 1 .

[0025] The overall structure of the invention (taking the integrated debugging module as an example) is as figure 2 As shown: the pan-tilt 2 is connected to the strut 4 through the ball joint bearing 3, so that the pan-tilt 2 can rotate around the spherical center of the ball joint bearing 3 with 3 degrees of freedom. The strut 4 is installed on the base 5 and can move up and down to adjust the installation height. Three support legs 6 are annularly installed on the base 5, and form a tripod together with the strut 4 and the base 5. The end section...

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Abstract

The invention provides a flight control debugging protecting device of a multi-rotor-wing unmanned plane. By the flight control debugging protecting device of the multi-rotor-wing unmanned plane, self-stabilization performance of a flight control system of the multi-rotor-wing unmanned plane can be debugged, and test safety is ensured. The flight control debugging protecting device of the multi-rotor-wing unmanned plane is based on a rigid body dynamics principle of flight of the multi-rotor-wing unmanned plane and comprises a triangular rack and four changeable flight control debugging modules; the movement type of the multi-rotor-wing unmanned plane is limited through a mechanical structure; three single degrees of freedom, including rolling, pitching and heading, of the flight control system of the unmanned plane can be debugged independently, and the three degrees of freedom can be debugged comprehensively; after control responses of the multi-rotor-wing unmanned plane are observed when the protecting device runs on different modules, actual performance of new skills and new methods which are used by the unmanned plane are clear; and self-stabilization of the flight control system can be subjected to functional partitioning, research and development engineering management is facilitated, debugging of the unmanned plane can be protected, possible property loss caused by blind trial flight is avoided, research and development risks and difficulties are reduced, and development of the industry of multi-rotor-wing unmanned planes is promoted.

Description

technical field [0001] The invention relates to the field of aviation technology, in particular to a flight control debugging protection device for a multi-rotor unmanned aerial vehicle. Background technique [0002] With the development of technology, multi-rotor UAVs have generally appeared in people's daily life. Especially in recent years, the development of the multi-rotor UAV industry has been highly active. From military to civilian use, from image acquisition, intelligence reconnaissance to ordinary photography, agricultural plant protection, logistics express, etc., multi-rotor UAVs can be called technology. Frontier, with great development potential and economic value. my country's multi-rotor UAV technology is very advanced, the multi-rotor UAV industry is very developed, there are a large number of active enterprises and scientific research institutes engaged in research in related fields, a large team of scientific research practitioners provides a solid techni...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G05D1/10
Inventor 杨福增李长骏伦佳琪杨鹏秦昊
Owner NORTHWEST A & F UNIV
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