Control Logic for Parameter Insensitivity and Disturbance Attenuation
- 1 July 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 5 (4) , 383-388
- https://doi.org/10.2514/3.56186
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Attitude Control of a Flexible SpacecraftJournal of Guidance and Control, 1980
- Optimal limited state variable feedback controllers for linear systemsIEEE Transactions on Automatic Control, 1971
- Minimax controller designIEEE Transactions on Automatic Control, 1968