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GPC-based stable reconfigurable control

  • Iowa State University
  • NASA Ames Research Center

Research output: Contribution to conferencePaperpeer-review

3 Scopus citations

Abstract

This paper presents development of multi-input multi-output (MIMO) Generalized Predictive Control (GPC) law and its application to reconfigurable control design in the event of actuator saturation. The stability of the GPC control law without reconfiguration is first established using Riccati-based approach and state-space formulation. A novel reconfiguration strategy is developed for the systems which have actuator redundancy and are faced with actuator saturation type failure. An elegant reconfigurable control design is presented with stability proof. A numerical example with application to reconfigurable flight control is presented to demonstrate the results presented in the paper.

Original languageEnglish
Pages821-828
Number of pages8
DOIs
StatePublished - 2003
Event2003 ASME International Mechanical Engineering Congress - Washington, DC, United States
Duration: Nov 15 2003Nov 21 2003

Conference

Conference2003 ASME International Mechanical Engineering Congress
Country/TerritoryUnited States
CityWashington, DC
Period11/15/0311/21/03

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