Robust nonlinear H_inf decoupling control of flight vehicle in hovering

Ciann Dong Yang, Chien Chung Kung

研究成果: Conference article

9 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

    指紋

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering
  • Modelling and Simulation
  • Control and Optimization

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