Robust stability of unified singularly perturbed feedback systems

H. Singh, R. H. Brown, D. S. Naidu, J. A. Heinen

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

A method for decomposition of unified state feedback singularly perturbed systems is presented. Based on the small gain theorem, a sufficient condition for robust stability is derived such that the composite state feedback renders the closed-loop singularly perturbed system asymptotically stable. With this method there is no need to consider two different (continuous/discrete) domains. An F-4 fighter aircraft example is given to illustrate the methodology.

Original languageEnglish (US)
Title of host publicationGuidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
Pages820-825
Number of pages6
StatePublished - Jan 1 1999
EventGuidance, Navigation, and Control Conference and Exhibit, 1999 - Portland, United States
Duration: Aug 9 1999Aug 11 1999

Other

OtherGuidance, Navigation, and Control Conference and Exhibit, 1999
CountryUnited States
CityPortland
Period8/9/998/11/99

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