Design of nonlinear control laws for high-angle-of-attack flight
- 1 July 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 17 (4) , 737-746
- https://doi.org/10.2514/3.21262
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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