ROBUST NONLINEAR CONTROLLER DESIGN FOR A LONGITUDINAL FLIGHT CONTROL PROBLEM

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

doi:10.1111/j.1934-6093.2000.tb00150.x

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ROBUST NONLINEAR CONTROLLER DESIGN FOR A LONGITUDINAL FLIGHT CONTROL PROBLEM

Journal article

Peer reviewed

ROBUST NONLINEAR CONTROLLER DESIGN FOR A LONGITUDINAL FLIGHT CONTROL PROBLEM

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

Asian journal of control, v 2(2), pp 111-121

Jun 2000

DOI: https://doi.org/10.1111/j.1934-6093.2000.tb00150.x

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Abstract

aircraft longitudinal flight control

nonlinear H∞ approximate I/O linearization problem

Nonlinear H∞ control

robust control

μ‐synthesis

ABSTRACT In this paper, the H∞ approximate I/O linearization formulation and μ‐synthesis are employed to design a nonlinear controller for an aircraft longitudinal flight control problem. We propose modified nonlinear H∞ controller formulas to approximately linearize the system and use μ‐synthesis to address tracking, regulation, and robustness issues.

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Title: ROBUST NONLINEAR CONTROLLER DESIGN FOR A LONGITUDINAL FLIGHT CONTROL PROBLEM
Creators: Shr‐Shiung Hu
B.C. Chang - Drexel University
H.H. Yeh - Wright-Patterson Air Force Base
H.G. Kwatny - Drexel University
Publication Details: Asian journal of control, v 2(2), pp 111-121
Publisher: Blackwell Publishing Ltd
Number of pages: 11
Resource Type: Journal article
Language: English
Academic Unit: Mechanical Engineering and Mechanics
Scopus ID: 2-s2.0-0012167940
Other Identifier: 991019174521804721

ROBUST NONLINEAR CONTROLLER DESIGN FOR A LONGITUDINAL FLIGHT CONTROL PROBLEM

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