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Fundamental relation of approximate receding-horizon optimization to the simple mass-spring-damper system

  • University of California at Santa Barbara

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

3 Scopus citations

Abstract

Model-error control synthesis is a nonlinear robust control approach that uses an optimal solution to cancel the effects of modelling errors and external disturbances on a system. The model error is determined by the approximated receding-horizon optimal solution. The future states are predicted by a repeated first-order Taylor series method or a higher-order Taylor series method. In this paper we show the fundamental relation between these two methods using the physical parameters, such as time constant and damping factor, of a simple mass-spring-damper system.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781563479786, 9781624100901
DOIs
StatePublished - 2003
EventAIAA Guidance, Navigation, and Control Conference and Exhibit 2003 - Austin, TX, United States
Duration: Aug 11 2003Aug 14 2003

Publication series

NameAIAA Guidance, Navigation, and Control Conference and Exhibit

Conference

ConferenceAIAA Guidance, Navigation, and Control Conference and Exhibit 2003
Country/TerritoryUnited States
CityAustin, TX
Period08/11/0308/14/03

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