A reduced-order H= controller is designed for full envelope flight control of a thrust vectoring aircraft. Structured singular values and nonlinear simulations are used to analyze the robustness of the control system.
Parameter-robust flight control system for a flexible aircraft
โ Scribed by F. Kubica; T. Livet; X. Le Tron; A. Bucharles
- Publisher
- Elsevier Science
- Year
- 1995
- Tongue
- English
- Weight
- 555 KB
- Volume
- 3
- Category
- Article
- ISSN
- 0967-0661
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