SDRE AUTOPILOT FOR DUAL CONTROLLED MISSILES
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Published:2007
Issue:7
Volume:40
Page:750-755
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ISSN:1474-6670
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Container-title:IFAC Proceedings Volumes
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language:en
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Short-container-title:IFAC Proceedings Volumes
Reference4 articles.
1. Mracek, C.P. and J.R. Cloutier, “Full Envelope Missile Longitudinal Autopilot Using the State-Dependent Riccati Equation Method”, AIAA Guidance, Navigation and Conference, New Orleans LA, Aug 1997.
2. Automatic Control of Aircraft and Missiles;Blakelock,1991
3. Dynamics of Atmospheric Flight;Etkin,1972
4. Mracek, C.P. and D.B. Ridgely, “Optimal Control Solution for Dual (Tail and Canard) Control Missiles”, AIAA Guidance, Navigation and Conference, Keystone CO, Aug 2006.
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