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
QFT design of multi-loop nonlinear control systems
✍ Scribed by Alfonso Baños; Isaac Horowitz
- Publisher
- John Wiley and Sons
- Year
- 2000
- Tongue
- English
- Weight
- 241 KB
- Volume
- 10
- Category
- Article
- ISSN
- 1049-8923
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