Nonlinear robust controller design based on H∞ I/O linearization and μ-synthesis

Shr-Shiung Hu; B.C. Chang; H.H. Yeh; H.G. Kwatny

doi:10.1016/S1474-6670(17)56526-X

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Nonlinear robust controller design based on H∞ I/O linearization and μ-synthesis

Journal article

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Nonlinear robust controller design based on H∞ I/O linearization and μ-synthesis

Shr-Shiung Hu, B.C. Chang, H.H. Yeh and H.G. Kwatny

IFAC Proceedings Volumes, v 32(2), pp 3085-3090

Jul 1999

DOI: https://doi.org/10.1016/S1474-6670(17)56526-X

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Abstract

flight control

nonlinear control

robust control

In this paper, an H∞ approximate I/O linearization and the μ-synthesis will be employed to obtain a nonlinear robust controller for an aircraft longitudinal flight control problem. Simulations of the tracking responses of the closed-loop system will be also included.

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Title: Nonlinear robust controller design based on H∞ I/O linearization and μ-synthesis
Creators: Shr-Shiung Hu - 202nd Arsenal Combined Service Forces P. O. Box 90582 Nankang, Taiwan
B.C. Chang - Drexel University
H.H. Yeh - Wright-Patterson Air Force Base
H.G. Kwatny - Drexel University
Publication Details: IFAC Proceedings Volumes, v 32(2), pp 3085-3090
Publisher: Elsevier
Resource Type: Journal article
Language: English
Academic Unit: Mechanical Engineering and Mechanics
Other Identifier: 991019205714304721

Nonlinear robust controller design based on H∞ I/O linearization and μ-synthesis

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