Abstract
This paper studies the reliable and robust H∞ (RRH∞) flight controller. design, based on the iterative linear matrix inequality (ILMI) approach, for a bank-angle tracking maneuver of a jet transport aircraft. While meeting certain robustness properties, the RRH∞ flight controller explicitly considers a reliability property which tolerates the loss of actuator effectiveness. The RRH∞ flight controller also seeks to optimize the nominal performance of the resultant closed-loop system. Simulation results demonstrate good performance using the RRH∞ flight controller scheme.
Original language | English |
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Pages (from-to) | 229-234 |
Number of pages | 6 |
Journal | Proceedings of the IEEE Conference on Decision and Control |
Volume | 1 |
Publication status | Published - 2001 |
Externally published | Yes |
Event | 40th IEEE Conference on Decision and Control (CDC) - Orlando, FL, United States Duration: 4 Dec 2001 → 7 Dec 2001 |
Keywords
- H design
- Reliable design
ASJC Scopus subject areas
- Control and Systems Engineering
- Modelling and Simulation
- Control and Optimization