Hayabusa2 Mission Solar Conjunction Phase for Hovering Satellite: Trajectory Design, Navigation and Post-Operation Evaluation
Hayabusa2 Mission Solar Conjunction Phase for Hovering Satellite: Trajectory Design, Navigation and Post-Operation Evaluation
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隼鸟二号任务悬停卫星太阳合相阶段:轨迹设计、导航和运行后评估
DOI:
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发表时间:
2019
期刊:
影响因子:
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通讯作者:
T. Yamaguchi
中科院分区:
文献类型:
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作者:
S. Soldini;Y. Tsuda;T. Yamaguchi