Nonlinear H∞ decoupling control for hovering helicopter

Ciann-Dong Yang, Wen Hsiung Liu, Chien Chung Kung

Research output: Contribution to journalArticle

19 Citations (Scopus)

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 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.

Original languageEnglish
Pages (from-to)4353-4358
Number of pages6
JournalProceedings of the American Control Conference
Volume6
Publication statusPublished - 2002

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Helicopters
Controllers

All Science Journal Classification (ASJC) codes

  • Control and Systems Engineering

Cite this

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Nonlinear H∞ decoupling control for hovering helicopter. / Yang, Ciann-Dong; Liu, Wen Hsiung; Kung, Chien Chung.

In: Proceedings of the American Control Conference, Vol. 6, 2002, p. 4353-4358.

Research output: Contribution to journalArticle

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