Abstract:
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-...Show MoreMetadata
Abstract:
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/sub /spl infin// controller designed for hovering helicopters can be exactly separated into two three degree-of-freedom controllers, one for translational motion and the other for rotational motion.
Date of Conference: 08-10 May 2002
Date Added to IEEE Xplore: 07 November 2002
Print ISBN:0-7803-7298-0
Print ISSN: 0743-1619
Contents 