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PILOT-VEHICLE SEMI-PHYSICAL SIMULATION STUDY OF DECOUPLING CONTROL FOR AIRCRAFT TF/TA PENETRATION
Sun Baoting;Chen Yanyang
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 1995, (3): 30 -35 . 

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341