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J-GLOBAL ID：201702222980954913   Reference number：17A0066606

A Satellite Orbit Determination Method of Injection Segment Data Based on Velocity Increment Correction

速度増分補正に基づく衛星入力軌道決定のための新しい方法を提案した。【JST・京大機械翻訳】

Author (5)： Mao Yongxing (China Satellite Maritime Tracking and Control Department) ,  Ma Jingyuan (Purple Mountain Observatory, Chinese Academy of Sciences) ,  Zhong Dean (China Satellite Maritime Tracking and Control Department) ,  Ni Xiaoqiu (China Satellite Maritime Tracking and Control Department) ,  Xiang Jie (China Satellite Maritime Tracking and Control Department)
Material： Yuhang Xuebao  (Journal of Astronautics)
Volume： 37  Issue： 9  Page： 1049-1055  Publication year： 2016 
JST Material Number： C2003A  ISSN： 1000-1328  Document type： Article
Article type： 原著論文  Country of issue： China (CHN)  Language： CHINESE (ZH)

Abstract/Point： Based on the traditional orbit...

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Thesaurus term： numerical integration ,  simulation ,  *orbit determination

Author keywords (4)： Earth-to-moon transfer orbit ,  Velocity increment correction ,  Precise orbit determination ,  Orbit improvement

JST classification (1)： Motion and orbit of space crafts  (QK02060W)

Terms in the title (3)： 衛星 ,  軌道決定 ,  提案