Abstract:
Although longitudinal and lateral dynamics of helicopters in hovering are highly nonlinear and severely coupled, we show that the nonlinear six degree-of-freedom H/sub /s...Show MoreMetadata
Abstract:
Although longitudinal and lateral dynamics of helicopters in hovering are highly nonlinear and severely coupled, we show that the nonlinear six degree-of-freedom H/sub /spl infin// 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.
Date of Conference: 10-13 December 2002
Date Added to IEEE Xplore: 10 March 2003
Print ISBN:0-7803-7516-5
Print ISSN: 0191-2216
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