Precise guidance and landing strategy of space probe by using multiple markers in asteroid exploration mission

Naoko Ogawa, Fuyuto Terui, Jun'ichiro Kawaguchi

研究成果: Conference contribution

4 被引用数 (Scopus)

抄録

This paper proposes a novel strategy for a space probe to descent and land on the asteroid surface with high accuracy of a few meters by utilizing several artificial markers deployed from the probe. Results of a numerical experiment indicated that the proposed method showed higher performance than conventional one. It will allow us to guide the probe with high mobility to the desired points such as small craters, which will be of great significance for understanding local geology and geography of the asteroid, or avoiding boulders and too rough regions.

本文言語English
ホスト出版物のタイトルASTRODYNAMICS 2011 - Advances in the Astronautical Sciences
ホスト出版物のサブタイトルProceedings of the AAS/AIAA Astrodynamics Specialist Conference
ページ3817-3832
ページ数16
出版ステータスPublished - 2012
外部発表はい
イベント2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011 - Girdwood, AK, United States
継続期間: 2011 7 312011 8 4

出版物シリーズ

名前Advances in the Astronautical Sciences
142
ISSN(印刷版)0065-3438

Conference

Conference2011 AAS/AIAA Astrodynamics Specialist Conference, ASTRODYNAMICS 2011
国/地域United States
CityGirdwood, AK
Period11/7/3111/8/4

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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