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.
|頁（從 - 到）||4486-4491|
|期刊||Proceedings of the IEEE Conference on Decision and Control|
|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 10 → 2002 十二月 13
All Science Journal Classification (ASJC) codes