Rendezvous to asteroid with highly uncertain ephemeris: Hayabusa2's Ryugu-approach operation result

被引:18
作者
Tsuda, Yuichi [1 ]
Takeuchi, Hiroshi [1 ]
Ogawa, Naoko [1 ]
Ono, Go [2 ]
Kikuchi, Shota [1 ]
Oki, Yusuke [3 ]
Ishiguro, Masateru [4 ]
Kuroda, Daisuke [5 ]
Urakawa, Seitaro [6 ]
Okumura, Shin-ichiro [6 ]
机构
[1] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Sagamihara 2525210, Japan
[2] Japan Aerosp Explorat Agcy, Res & Dev Directorate, Sagamihara 2525210, Japan
[3] Japan Aerosp Explorat Agcy, Res & Dev Directorate, Tsukuba 3058505, Japan
[4] Seoul Natl Univ, Seoul 08826, South Korea
[5] Kyoto Univ, Okayama Observ, Asakuchi 7190232, Japan
[6] Japan Spaceguard Assoc, Bisei 7141411, Japan
关键词
solar system exploration; sample return; optical navigation; trajectory optimization; spacecraft guidance; CALIBRATION; MISSION;
D O I
10.1007/s42064-020-0074-9
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This paper describes the guidance and navigation technique used by Hayabusa2 for the asteroid rendezvous operation to reach Ryugu. The operation results, including the achieved guidance and navigation performance, are also summarized. Multiple assessment and navigation teams worked closely to provide reliable navigation solutions with a short solution delivery cycle. Although the uncertainty of the Ryugu's ephemeris was considerable before Hayabusa2's arrival, a combination of radiometric-optical hybrid navigation and a stochastic-constrained optimum guidance method was able to achieve an accuracy of less than 100 m and 1 cm/s, and the arrival was precisely timed.
引用
收藏
页码:137 / 147
页数:11
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