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Cyclic pursuit control method design for spacecraft formation configuration adjustment
YANG Huixin
ACTA AERONAUTICAET ASTRONAUTICA SINICA . 2020, (S2): 724311 -724311 .  DOI: 10.7527/S1000-6893.2020.24311

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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