A Sliding Mode Static Output Feedback Controller Based on Linear Matrix Inequalities Applied to an Aircraft System-Reference-Cited by-同舟云学术

A Sliding Mode Static Output Feedback Controller Based on Linear Matrix Inequalities Applied to an Aircraft System

Published:2000-01-31 Issue:4 Volume:122 Page:656-662
ISSN:0022-0434
Container-title:Journal of Dynamic Systems, Measurement, and Control
language:en
Short-container-title:

Author:

Edwards Christopher¹,Spurgeon Sarah K.¹,Akoachere Ashu¹

Affiliation:

1. Control Systems Research, Department of Engineering, University of Leicester, Leicester LE1 7RH, United Kingdom

Abstract

This paper presents a variable structure control design methodology for multi-input uncertain dynamic systems using only plant output information. Static output feedback is utilized in the design of the switching surface using a Linear Matrix Inequality approach recently proposed in the literature. A novel LMI based optimization approach is subsequently employed in the construction of the control law to guarantee that a sliding motion takes place. The efficacy of the algorithms is demonstrated on a nontrivial design example—an aircraft system representation which includes the flexible modes of the airframe. [S0022-0434(00)00204-5]

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Link

http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/122/4/656/5779917/656_1.pdf

Reference15 articles.

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3. Hui, S., and Z˙ak, S., 1993, “Robust output feedback stabilisation of uncertain dynamic systems with bounded controllers,” Int. J. Robust Nonlinear Control, 3, pp. 115–132.

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5. Heck, B., Yallapragada, S., and Fan, M., 1995, “Numerical methods to design the reaching phase of output feedback variable structure control,” Automatica, 31, pp. 275–279.

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