Decoupling control for hovering flight vehicle with parameter uncertainties

Ciann Dong Yang, Wen Hsiung Liu, Po Wei Chang, Hung Jen Weng

研究成果: Conference contribution

3 引文 斯高帕斯(Scopus)

摘要

This paper proposes a new approach to consider nonlinear H control of hovering vehicles described by six-degree-of-freedom nonlinear dynamics with plant uncertainties due to the variation of moments of inertia caused by fuel consumption and/or payload operation. Taking into account nonlinear effect, plant uncertainty, and exogenous disturbances caused by wind gust, we show in this paper that the six-degree-of-freedom nonlinear H controller can be exactly decoupled into two three-degree-of-freedom controllers, one for translational motion and the other for rotational motion, even though longitudinal and lateral dynamics of flight vehicle in hover are highly nonlinear and severely coupled.

原文English
主出版物標題Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006
發行者American Institute of Aeronautics and Astronautics Inc.
頁面786-798
頁數13
ISBN(列印)1563478196, 9781563478192
DOIs
出版狀態Published - 2006 一月 1
事件AIAA Guidance, Navigation, and Control Conference 2006 - Keystone, CO, United States
持續時間: 2006 八月 212006 八月 24

出版系列

名字Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference 2006
2

Other

OtherAIAA Guidance, Navigation, and Control Conference 2006
國家United States
城市Keystone, CO
期間06-08-2106-08-24

All Science Journal Classification (ASJC) codes

  • Engineering(all)

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