Approximations for Quantitative Feedback Theory Designs
- 1 July 1997
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 20 (4) , 828-831
- https://doi.org/10.2514/2.4122
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Improved design technique for uncertain multiple-input-multiple-output feedback systems†International Journal of Control, 1982