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Linear stability analysis of model error control synthesis

  • Texas A&M University

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

9 Scopus citations

Abstract

Recently, a new approach for the robust control of nonlinear systems was presented. This approach, called Model Error Control Synthesis, employs an optimal real-time nonlinear estimator to determine model error corrections to the control input of a sliding mode controller using a one time-step ahead technique. Control compensation is achieved by using the estimated model error as a signal synthesis adaptive correction to the nominal control input so that maximum performance is achieved in the face of extreme model uncertainty and disturbance inputs. In this paper Model Error Control Synthesis is applied to a simple second order linear mass-spring-damper system and a higher order benchmark problem. A robustness analysis is performed for the mass-spring-damper system. The proof of the closed loop stability is derived using a Padé approximation for the time delay. It is shown that the weighting coefficient for the model error correction in the associated cost function cannot be set to zero since this gives a non-minimum phase system in the closed-loop response, and the control law itself is not asymptotically stable. Simulations are used to verify theoretical results.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781563479786
DOIs
StatePublished - 2000
EventAIAA Guidance, Navigation, and Control Conference and Exhibit 2000 - Dever, CO, United States
Duration: Aug 14 2000Aug 17 2000

Publication series

NameAIAA Guidance, Navigation, and Control Conference and Exhibit

Conference

ConferenceAIAA Guidance, Navigation, and Control Conference and Exhibit 2000
Country/TerritoryUnited States
CityDever, CO
Period08/14/0008/17/00

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