Full envelope multivariable control law synthesis for a high-performance test aircraft
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 16 (5) , 948-955
- https://doi.org/10.2514/3.21106
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Multivariable variable-structure adaptive model-following control systemsIEE Proceedings D Control Theory and Applications, 1982