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[American Institute of Aeronautics and Astronautics Guidance, Navigation, and Control Conference - New Orleans,LA,U.S.A. (11 August 1997 - 13 August 1997)] Guidance, Navigation, and Control Conference - Full envelope missile longitudinal autopilot design using the state-dependent Riccati equation method
Mracek, Curtis, Cloutier, James, Cloutier, James, Mracek, CurtisYear:
1997
Language:
english
DOI:
10.2514/6.1997-3767
File:
PDF, 584 KB
english, 1997