Automatic take-off control method and automatic landing control method of hand-throwing type solar fixed-wing unmanned aerial vehicle

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Automatic take-off control method and automatic landing control method of hand-throwing type solar fixed-wing unmanned aerial vehicle

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LI KE / ZHANG YUXIANG / DUAN PENGYU / LYU XINYANG / HUANG MAN / SONG HANQI / HUI YUHANG

The invention provides an automatic landing control method of a hand-throwing type solar fixed-wing unmanned aerial vehicle. The method has the advantages that a landing module is divided into three modules, namely a main control module, an initial-section landing control module and a final-section landing control module, so that the mutual coupling is less, and the expansion and improvement of the functions of each module are facilitated; in the landing process, the three modules all have re-flight judgment, so that the judgment of the aircraft on the height and the re-flight condition can be greatly improved, and the hidden danger of loss caused by forced landing of the unmanned aerial vehicle due to inaccurate judgment is prevented.

本发明提供了一种手抛式太阳能固定翼无人机的自动降落控制方法，其优点包括：降落模块分成三个模块，主控制模块、出段降落控制模块、终段降落控制模块，相互耦合较少，方便针对各模块功能的扩展与改进；降落过程三个模块中都有复飞判断，能够较大提升飞机对于自身高度与复飞条件的判断，防止无人机因为判断不准、强行着陆带来的损失隐患。

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Title :

Automatic take-off control method and automatic landing control method of hand-throwing type solar fixed-wing unmanned aerial vehicle

Additional title:

手抛式太阳能固定翼无人机的自动起飞控制方法与自动降落控制方法

Contributors:

LI KE (author) / ZHANG YUXIANG (author) / DUAN PENGYU (author) / LYU XINYANG (author) / HUANG MAN (author) / SONG HANQI (author) / HUI YUHANG (author)

Publication date :

2021-05-28

Type of media :

Patent

Type of material :

Electronic Resource

Language :

Chinese

Classification :

IPC:

B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen