
A Method to Calculate the Short-Time Orbit Maneuver Acceleration Based on the Satellite Ephemeris
CUI Shuang-xing, YANG Zhi-tao, LIU wei, WANG Rong-lan, XIANG Kai-heng, HE Quan, WU Zhong-hao
A Method to Calculate the Short-Time Orbit Maneuver Acceleration Based on the Satellite Ephemeris
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