Short Takeoff and Vertical Landing Aircraft Deceleration Transition Control Based on Adaptive Control
Addressing the issues of nonlinearity, control redundancy and coupling, and system uncertainties in the deceleration transition process from level flight to hover in short takeoff and vertical landing (STOVL) aircraft, this paper establishes a six-degree-of-freedom nonlinear mathematical model for t...
Αποθηκεύτηκε σε:
| Κύριοι συγγραφείς: | , , , , |
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| Μορφή: | Artigo |
| Γλώσσα: | Inglês |
| Έκδοση: |
World Scientific Publishing Co Pte Ltd
2024-11-01
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| Σειρά: | Guidance, Navigation and Control |
| Θέματα: | |
| Διαθέσιμο Online: | https://www.worldscientific.com/doi/10.1142/S2737480724500195 |
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