Robust nonlinear H_inf decoupling control of flight vehicle in hovering

Ciann Dong Yang, Chien Chung Kung

研究成果: Conference article同行評審

10 引文 斯高帕斯(Scopus)

摘要

Although longitudinal and lateral dynamics of helicopters in hovering are highly nonlinear and severely coupled, we will show in this paper that the nonlinear six degree-of-freedom H controller designed for hovering helicopter can be exactly separated into two three degree-of-freedom controllers, one for translational motion and the other for rotational motion.

原文English
頁(從 - 到)4486-4491
頁數6
期刊Proceedings of the IEEE Conference on Decision and Control
4
出版狀態Published - 2002 十二月 1
事件41st IEEE Conference on Decision and Control - Las Vegas, NV, United States
持續時間: 2002 十二月 102002 十二月 13

All Science Journal Classification (ASJC) codes

  • 控制與系統工程
  • 建模與模擬
  • 控制和優化

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