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Reaction jet and Aerodynamics Compound Control Missile Autopilot Design Based on Adaptive Fuzzy Sliding Mode Control via Backstepping
CHEN Yu;DONG Chao-yang;WANG Qing;ZHANG Ming-lian
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2007, (增): 141 -145 . 

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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