High-Performance, Robust, Bank-to-Turn Missile Autopilot Design
- 1 January 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 18 (1) , 46-53
- https://doi.org/10.2514/3.56655
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Fast computation of achievable feedback performance in mixed sensitivityH^{∞}designIEEE Transactions on Automatic Control, 1987
- Robust missile autopilot design using a generalized singular optimalcontrol techniqueJournal of Guidance, Control, and Dynamics, 1985