Anti-swing Coordinated Control of the UAV Wing Folding During the Aerial Recovery Process

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Anti-swing Coordinated Control of the UAV Wing Folding During the Aerial Recovery Process

Liu, Yiheng / Wang, Honglun / Wang, Yanxiang / Fan, Jiaxuan

In the process of UAV aerial recovery, the UAV needs to fold its wings, which will lead to a sharp drop in the lift and cause the cable to sway. Aiming at this problem, an anti-swing coordinated control method of wing folding based on quadratic programming control allocation is proposed. It can make full use of the grid rudder of the drogue to compensate the lift lost caused by wing folding and use quadratic programming to allocate the rudder deflection angle that can not only satisfy the moment balance, but also satisfy the force balance, so as to realize the coordinated control of the drogue grid rudder and the UAV rudder surface. Simulations are conducted to verify the effectiveness of the proposed control method.

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Dokumentinformationen

Titel :

Anti-swing Coordinated Control of the UAV Wing Folding During the Aerial Recovery Process

Weitere Titelangaben:

Lect. Notes Electrical Eng.

Beteiligte:

Yan, Liang (Herausgeber:in) / Duan, Haibin (Herausgeber:in) / Deng, Yimin (Herausgeber:in) / Liu, Yiheng (Autor:in) / Wang, Honglun (Autor:in) / Wang, Yanxiang (Autor:in) / Fan, Jiaxuan (Autor:in)

Kongress:

International Conference on Guidance, Navigation and Control ; 2022 ; Harbin, China August 05, 2022 - August 07, 2022

Erschienen in:

Advances in Guidance, Navigation and Control ; Kapitel : 503 ; 5212-5220

Lecture Notes in Electrical Engineering ; 845

Erscheinungsdatum :

2023-01-31

Format / Umfang :

9 pages

ISBN :

978-981-19-6613-2 , 978-981-19-6612-5

ISSN :