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DESIGN OF GUIDANCE AND CONTROL SYSTEM FOR HIGH SPEED REENTRY AEROCRAFT
LIAN Bao-hua;CUI Ping-yuan;CUI Hu-tao
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2002, (2): 115 -119 . 

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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