Hayabusa2’s station-keeping operation in the proximity of the asteroid Ryugu

查看全文 作　　者：Yuto [1]Takei;Takanao [1]Saiki;Yukio [1,2]Yamamoto;Yuya [1]Mimasu;Hiroshi [1,2]Takeuchi;Hitoshi [1]Ikeda;Naoko [1]Ogawa;Fuyuto [1]Terui;Go [1]Ono;Kent [1]Yoshikawa;Tadateru [4]Takahashi;Hirotaka [1]Sawada;Chikako [1]Hirose;Shota [1]Kikuchi;Atsushi [1]Fuji;Takahiro [1,2]Iwata;Satoru [1]Nakazawa;Masahiko [1]Hayakawa;Ryudo [1]Tsukizaki;Satoshi [1,2]Tanaka;Masanori [1]Matsushita;Osamu [1]Mori;Daiki [1]Koda;Takanobu [1]Shimada;Masanobu [1,2]Ozaki;Masanao [1,2]Abe;Satoshi [1]Hosoda;Tatsuaki [1]Okada;Hajime [1,2]Yano;Takaaki [3]Kato;Seiji [1]Yasuda;Kota [4]Matsushima;Tetsuya [4]Masuda;Makoto [1,2]Yoshikawa;Yuichi [1,2]Tsuda

机构地区：[1]Japan Aerospace Exploration Agency,Sagarmihara 252-5210,Japan;[2]The Graduate University for Advanced Studies,Sagarmihara 252-5210,Japan;[3]NEC Aerospace Systems,Ltd,Fruchu 183-8502,Japan;[4]NEC Corporation,Puchu 183-8501,Japan

出　　处：《Astrodynamics》索引2020年第4卷第4期,共27页

摘　　要：The Japanese interplanetary probe Hayabusa2 was launched on December 3,2014 and the probe arrived at the vicinity of asteroid 162173 Ryugu on June 27,2018.During its 1.4 years of asteroid proximity phase,the probe successfully accomplished numbers of record-breaking achievements including two touchdowns and one artificial cratering experiment,which are highly expected to have secured surface and subsurface samples from the asteroid inside its sample container for the first time in history.The Hayabusa2 spacecraft was designed not to orbit but to hover above the asteroid along the sub Earth line.This orbital and geometrical configuration allows the spacecraft to utilize its high-gain antennas for telecommunication with the ground station on Earth while pointing its scientific observation and navigation sensors at the asteroid.This paper focuses on the regular station-keeping operation of Hayabusa2,which is called“home position”(HP)-keeping operation.First,together with the spacecraft design,an operation scheme called HP navigation(HPNAV),which includes a daily trajectory control and scientific observations as regular activities,is introduced.Following the description on the guidance,navigation,and control design as well as the framework of optical and radiometric navigation,the results of the HP-keeping operation including trajectory estimation and delta-V planning during the entire asteroid proximity phase are summarized and evaluated as a first report.Consequently,this paper states that the HP.keeping operation in the framework of HPNAV had succeeded without critical incidents,and the number of trajectory control delta-V was planned fficiently throughout the period. 关键词：small body mission station-keeping guidance,navigation,and control(GNC) optical and radiometric navigation

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Hayabusa2’s station-keeping operation in the proximity of the asteroid Ryugu

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