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Trajectory estimation method of missile in boost phase using optimal knots spline
ZHANG Tao, FAN Shiwei, XUE Yonghong, DING Yonghe
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2015, (9): 3027 -3033 .  DOI: 10.7527/S1000-6893.2015.0049

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341