An aircraft's response to control inputs varies widely throughout its full flight envelope. Furthermore, the aircraft configuration impacts control response through variations in centre of gravity and moments of inertia. Quantitative feedback theory (QFT) is a robust control system design method whi
โฆ LIBER โฆ
FAULT TOLERANT CONTROL SYSTEM: QFT DESIGN
โ Scribed by M. S. Keating; M. Pachter; C. H. Houpis
- Publisher
- John Wiley and Sons
- Year
- 1997
- Tongue
- English
- Weight
- 554 KB
- Volume
- 7
- Category
- Article
- ISSN
- 1049-8923
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โฆ Synopsis
This paper addresses flight control system synthesis and the accommodation of controlled plant variation in an aircraft design envelope by using the frequency domain based quantitative feedback theory (QFT) robust control system design method. Plant variations considered include varying flight conditions in the flight envelope and damage to aerodynamic control surfaces. A robust flight control system is designed for the aircraft's longitudinal and lateral directional channels and validated with simulations containing nonlinear saturation elements.
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