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 language | English |
|---|---|
| Pages | 821-828 |
| Number of pages | 8 |
| DOIs | |
| State | Published - 2003 |
| Event | 2003 ASME International Mechanical Engineering Congress - Washington, DC, United States Duration: Nov 15 2003 → Nov 21 2003 |
Conference
| Conference | 2003 ASME International Mechanical Engineering Congress |
|---|---|
| Country/Territory | United States |
| City | Washington, DC |
| Period | 11/15/03 → 11/21/03 |
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