Autopilot design for a missile with reaction-jet using coefficient diagram method
Authors:
- 6 August 2001
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
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- Agile Missile Dynamics and ControlJournal of Guidance, Control, and Dynamics, 1998
- Coefficient Diagram Method as Applied to the Attitude Control of Controlled-Bias-Momentum SatelliteIFAC Proceedings Volumes, 1994
- Simultaneous reaction jet and aerodynamic control of missile systems1993
- Radome induced miss distance in aerodynamically controlled homing missiles1984