| Citation: | Xing Lidan, Chen Wanchun, Yin Xinglianget al. Autopilot design for missile controlled by lateral thrust/aero force using combined optimal/classical approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 921-924. (in Chinese)
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[1] Chadwick W R, Augmentation of high-altitude maneuver performance of a tail-controlled missile using lateral thrust .ADA328973, 1995 [2] Schroeder W K, Liu K. An appropriate application of fuzzy logic: a missile autopilot for dual control implementation Proceedings of the 1994 IEEE International Symposium on Intelligent Control. 1994:93-98 [3] Hirokawa R, Sato K. Autopilot design for a missile with reaction-jet using coefficient diagram method . AIAA-2001-4162,2001 [4] 程凤舟,拦截战术弹道导弹末段导引和复合控制研究 . 西安:西北工业大学航天工程学院,2002 Cheng Fengzhou, Studies of guidance and combined control in terminal phase when intercepting tactical ballistic missile . Xi-an:Collego of Astronautics,Northwestern Polytechnical University,2002(in Chinese) [5] Nesline William F, Wells Brian H, Paul Z. Combined optimal/classical approach to robust missile autopilot design[J]. Journal of Guidance and Control, 1979, 4(3):316-322 [6] Nesline William F, Paul Z. Why modern controllers can go unstable in practice[J]. Journal of Guidance, Control and Dynamics, 1984, 7(4):495-500 [7] Mracek Curtis P, Ridgely Brett D. Missile longitudinal autopilots: connections between optimal control and classical topologies . AIAA 2005-6381, 2005 [8] Mracek Curtis P, Ridgely Brett D. Missile longitudinal autopilots: comparison of multiple three loop topologies . AIAA 2005-6380, 2005
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Xing Lidan, Chen Wanchun, Yin Xinglianget al. Autopilot design for missile controlled by lateral thrust/aero force using combined optimal/classical approach[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 921-924. (in Chinese)
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