Gain-scheduled missile autopilot design using linear parameter varying transformations
- 1 March 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (2) , 256-263
- https://doi.org/10.2514/3.20997
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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