Full envelope flight control system design using quantitative feedback theory
- 1 January 1996
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 19 (1) , 23-29
- https://doi.org/10.2514/3.21575
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Full envelope multivariable control law synthesis for a high-performance test aircraftJournal of Guidance, Control, and Dynamics, 1993
- Quantitative feedback theoryIEE Proceedings D Control Theory and Applications, 1982