Agile Missile Dynamics and Control
- 1 May 1998
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 21 (3) , 441-449
- https://doi.org/10.2514/2.4256
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Comparison of six robustness tests evaluating missile autopilot robustness to uncertain aerodynamicsJournal of Guidance, Control, and Dynamics, 1992
- Integrated aerofin/thrust vector control for tactical missilesJournal of Propulsion and Power, 1991
- Aircraft Dynamics and Automatic ControlPublished by Walter de Gruyter GmbH ,1990
- Bank-to-turn missile autopilot design using loop transfer recoveryJournal of Guidance, Control, and Dynamics, 1990