Nonlinear control law with application to high angle-of-attack flight
- 1 May 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 15 (3) , 761-767
- https://doi.org/10.2514/3.20902
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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