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Missile Reaction jet/Aerodynamic Compound Control System Design Based onAdaptive Sliding Mode Control and Fuzzy Logic
Dong Chaoyang;Wang Feng;Gao Xiaoying;Wang Qing
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2008, (1): 165 -169 . 

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Total visits: 6658907 Today visits: 1341All copyright © editorial office of Chinese Journal of Aeronautics

All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341