Abstract
In this paper, we consider the reliable robust tracking controller design problem against actuator faults and control surface damages for a LTI system with input disturbance. First, models of actuator faults and control surface damages are presented. Then a reliable tracking controller design method is developed, which guarantees the closed-loop system stability, optimizes the tracking performance of the system in normal operations, and maintains an acceptable low-level tracking performance of the system in the event of actuator faults and/or control surface damages. This method is based on LQ/H∞ tracking performance indices and multi-objective optimization in terms of linear matrix inequalities. A numerical example of an F-16 aircraft model and its simulation results are given.
| Original language | English |
|---|---|
| Pages (from-to) | 3914-3919 |
| Number of pages | 6 |
| Journal | Proceedings of the IEEE Conference on Decision and Control |
| Volume | 4 |
| Publication status | Published - 2000 |
| Externally published | Yes |
| Event | 39th IEEE Confernce on Decision and Control - Sydney, NSW, Australia Duration: 12 Dec 2000 → 15 Dec 2000 |
Keywords
- Actuator faults
- Control surface damages
- Flight control
- LMI
- Reliable control
- Tracking
ASJC Scopus subject areas
- Control and Systems Engineering
- Modelling and Simulation
- Control and Optimization