Robust nonlinear H_inf decoupling control of flight vehicle in hovering

Ciann Dong Yang; Chien Chung Kung

Robust nonlinear H_inf decoupling control of flight vehicle in hovering

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

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)	4486-4491
Number of pages	6
Journal	Proceedings of the IEEE Conference on Decision and Control
Volume	4
Publication status	Published - 2002 Dec 1
Event	41st IEEE Conference on Decision and Control - Las Vegas, NV, United States Duration: 2002 Dec 10 → 2002 Dec 13

All Science Journal Classification (ASJC) codes

Control and Systems Engineering
Modelling and Simulation
Control and Optimization

Cite this

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title = "Robust nonlinear H_inf decoupling control of flight vehicle in hovering",

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.",

author = "Yang, {Ciann Dong} and Kung, {Chien Chung}",

year = "2002",

month = dec,

day = "1",

language = "English",

volume = "4",

pages = "4486--4491",

journal = "Proceedings of the IEEE Conference on Decision and Control",

issn = "0191-2216",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "41st IEEE Conference on Decision and Control ; Conference date: 10-12-2002 Through 13-12-2002",

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TY - JOUR

T1 - Robust nonlinear H_inf decoupling control of flight vehicle in hovering

AU - Yang, Ciann Dong

AU - Kung, Chien Chung

PY - 2002/12/1

Y1 - 2002/12/1

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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UR - http://www.scopus.com/inward/citedby.url?scp=0036994209&partnerID=8YFLogxK

M3 - Conference article

AN - SCOPUS:0036994209

SN - 0191-2216

VL - 4

SP - 4486

EP - 4491

JO - Proceedings of the IEEE Conference on Decision and Control

JF - Proceedings of the IEEE Conference on Decision and Control

T2 - 41st IEEE Conference on Decision and Control

Y2 - 10 December 2002 through 13 December 2002

ER -

Robust nonlinear H_inf decoupling control of flight vehicle in hovering

Abstract

All Science Journal Classification (ASJC) codes

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