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Minimum-fuel spacecraft transfer trajectories solved by direct/indirect hybrid continuation method
MENG Yazhe
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2017, (1): 320168 -320168 .  DOI: 10.7527/S1000-6893.2016.0183

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All copyright © editorial office of Chinese Journal of Aeronautics

Total visits: 6658907 Today visits: 1341