Adaptive Model Inversion Flight Control for Tilt-Rotor Aircraft
- 1 May 1999
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 22 (3) , 402-407
- https://doi.org/10.2514/2.4411
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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