Abstract
This paper studies the reliable robust tracking controller design problem against actuator faults and control surface impairment for aircraft. First, models of actuator faults and control surface impairment are presented. Then a reliable robust tracking controller design method is developed. This method is based on the mixed linear quadratic (LQ)//H ∞ tracking performance indexes and multiobjective optimization in terms of linear matrix inequalities. Flight control examples are given, and both linear and nonlinear simulations are given.
| Original language | English |
|---|---|
| Pages (from-to) | 76-89 |
| Number of pages | 14 |
| Journal | IEEE Transactions on Control Systems Technology |
| Volume | 10 |
| Issue number | 1 |
| DOIs | |
| Publication status | Published - Jan 2002 |
| Externally published | Yes |
Free Keywords
- Actuator faults
- Control surface impairment
- Flight control
- Linear matrix inequality (LMI)
- Reliable control
- Tracking
ASJC Scopus subject areas
- Control and Systems Engineering
- Electrical and Electronic Engineering
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