Non-fragile H∞ flight controller design for a high performance aircraft

Jiong Sang Yee; Guang Hong Yang; Jian Liang Wang

Non-fragile H_∞ flight controller design for a high performance aircraft

Jiong Sang Yee^*
, Guang Hong Yang
, Jian Liang Wang

^*Corresponding author for this work

Research output: Journal Publication › Conference article › peer-review

4 Citations (Scopus)

Abstract

This paper studies the design of non-fragile H_∞ output-feedback control for a high performance aircraft in executing a large bank-angle maneuver. The designed flight controller tolerates some multiplicative gain variations in the controller matrices. Through linear and nonlinear simulation results, the paper demonstrates the advantage of designing the non-fragile H_∞ flight controller for practical implementation.

Original language	English
Pages (from-to)	1857-1861
Number of pages	5
Journal	Proceedings of the American Control Conference
Volume	3
Publication status	Published - 2000
Externally published	Yes
Event	2000 American Control Conference - Chicago, IL, USA Duration: 28 Jun 2000 → 30 Jun 2000

ASJC Scopus subject areas

Electrical and Electronic Engineering

Cite this

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title = "Non-fragile H∞ flight controller design for a high performance aircraft",

abstract = "This paper studies the design of non-fragile H∞ output-feedback control for a high performance aircraft in executing a large bank-angle maneuver. The designed flight controller tolerates some multiplicative gain variations in the controller matrices. Through linear and nonlinear simulation results, the paper demonstrates the advantage of designing the non-fragile H∞ flight controller for practical implementation.",

author = "Yee, \{Jiong Sang\} and Yang, \{Guang Hong\} and Wang, \{Jian Liang\}",

year = "2000",

language = "English",

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journal = "Proceedings of the American Control Conference",

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AU - Yee, Jiong Sang

AU - Yang, Guang Hong

AU - Wang, Jian Liang

PY - 2000

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N2 - This paper studies the design of non-fragile H∞ output-feedback control for a high performance aircraft in executing a large bank-angle maneuver. The designed flight controller tolerates some multiplicative gain variations in the controller matrices. Through linear and nonlinear simulation results, the paper demonstrates the advantage of designing the non-fragile H∞ flight controller for practical implementation.

AB - This paper studies the design of non-fragile H∞ output-feedback control for a high performance aircraft in executing a large bank-angle maneuver. The designed flight controller tolerates some multiplicative gain variations in the controller matrices. Through linear and nonlinear simulation results, the paper demonstrates the advantage of designing the non-fragile H∞ flight controller for practical implementation.

UR - https://www.scopus.com/pages/publications/0034541950

M3 - Conference article

AN - SCOPUS:0034541950

SN - 0743-1619

VL - 3

SP - 1857

EP - 1861

JO - Proceedings of the American Control Conference

JF - Proceedings of the American Control Conference

T2 - 2000 American Control Conference

Y2 - 28 June 2000 through 30 June 2000

ER -

Non-fragile H_∞ flight controller design for a high performance aircraft

Abstract

ASJC Scopus subject areas

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