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

Ciann Dong Yang
, Chien Chung Kung

Department of Aeronautics and Astronautics

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

10 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)	4486-4491
Number of pages	6
Journal	Proceedings of the IEEE Conference on Decision and Control
Volume	4
Publication status	Published - 2002
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",

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

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.

UR - https://www.scopus.com/pages/publications/0036994209

UR - https://www.scopus.com/pages/publications/0036994209#tab=citedBy

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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