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Time and angle control guidance law based on optimal error dynamics
LI Bin, LIN Defu, HE Shaoming, BAI Bing
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2018, (11): 322215 -322225 .  DOI: 10.7527/S1000-6893.2018.22215

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341