Abstract
This paper studies the design of non-fragile H∞ output-feedback control for a high performance aircraft in executing a large bank-angle maneuver. The designed flight controller tolerates some multiplicative gain variations in the controller matrices. Through linear and nonlinear simulation results, the paper demonstrates the advantage of designing the non-fragile H∞ flight controller for practical implementation.
Original language | English |
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Pages (from-to) | 1857-1861 |
Number of pages | 5 |
Journal | Proceedings of the American Control Conference |
Volume | 3 |
Publication status | Published - 2000 |
Externally published | Yes |
Event | 2000 American Control Conference - Chicago, IL, USA Duration: 28 Jun 2000 → 30 Jun 2000 |
ASJC Scopus subject areas
- Electrical and Electronic Engineering