High performance linear-quadratic and H-infinity designs for a 'supermaneuverable' aircraft
- 1 January 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 14 (1) , 157-165
- https://doi.org/10.2514/3.20617
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Development and evaluation of precision control modes for fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976