Nonlinear H∞ decoupling control for hovering helicopter

Ciann Dong Yang; Wen Hsiung Liu; Chien Chung Kung

Nonlinear H_∞ decoupling control for hovering helicopter

Ciann Dong Yang, Wen Hsiung Liu, Chien Chung Kung

Department of Aeronautics and Astronautics

Research output: Contribution to journal › Conference article › peer-review

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 language	English
Pages (from-to)	4353-4358
Number of pages	6
Journal	Proceedings of the American Control Conference
Volume	6
Publication status	Published - 2002
Event	2002 American Control COnference - Anchorage, AK, United States Duration: 2002 May 8 → 2002 May 10

All Science Journal Classification (ASJC) codes

Electrical and Electronic Engineering

Cite this

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title = "Nonlinear H∞ decoupling control for hovering helicopter",

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.",

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journal = "Proceedings of the American Control Conference",

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AU - Yang, Ciann Dong

AU - Liu, Wen Hsiung

AU - Kung, Chien Chung

PY - 2002

Y1 - 2002

N2 - 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.

AB - 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.

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M3 - Conference article

AN - SCOPUS:0036061306

SN - 0743-1619

VL - 6

SP - 4353

EP - 4358

JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

T2 - 2002 American Control COnference

Y2 - 8 May 2002 through 10 May 2002

ER -

Nonlinear H_∞ decoupling control for hovering helicopter

Abstract

All Science Journal Classification (ASJC) codes

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