Agile missile dynamics and control
- 29 July 1996
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamicsJournal of Guidance, Control, and Dynamics, 1992
- Robust hover control for a short takeoff/vertical landing aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Bank-to-turn missile autopilot design using loop transfer recoveryJournal of Guidance, Control, and Dynamics, 1990