WEKO3
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Study on high accurate navigation and guidance for the lunar soft landing experimental vehicle (SELENE-B)
https://jaxa.repo.nii.ac.jp/records/7725
https://jaxa.repo.nii.ac.jp/records/7725d47c9d62-5727-46c3-82de-e71d8a32d267
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Study on high accurate navigation and guidance for the lunar soft landing experimental vehicle (SELENE-B) | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | SELENE-B | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月着陸 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地質調査 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軟着陸 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 月表面 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 誘導・航法 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 信頼性 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 数値シミュレーション | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | SELENE-B | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lunar landing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | geological survey | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | soft landing | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | lunar surface | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | navigation and guidance | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | reliability | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | numerical simulation | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | 月軟着陸実験機(SELENE-B)高精度着陸航法誘導制御系に関する研究 | |||||
著者 |
石島, 義之
× 石島, 義之× 山本, 昌幸× 林, 健太郎× 澤井, 秀次郎× 橋本, 樹明× 佐々, 修一× 藤原, 健× 濱田, 吉郎× Ishijima, Yoshiyuki× Yamamoto, Masayuki× Hayashi, Kentaro× Sawai, Shujiro× Hashimoto, Tatsuaki× Sasa, Shuichi× Fujiwara, Takeshi× Hamada, Yoshiro |
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著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙開発事業団 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
宇宙科学研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
National Space Development Agency of Japan | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
平成15年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers p. 150-155, 発行日 2004-02 |
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抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 月面上の特定の地点におけるサイエンスミッションを実現するため、月軟着陸実験機(SELENE-B)では高精度かつ安全な着陸が要求されている。本研究では、画像センサや高度計を利用した対月航法により実現される着陸時航法精度について共分散解析検討結果を示すとともに、ON/OFFスラスタ駆動制約下で高精度にダウンレンジ/クロスレンジを誘導する動力降下誘導アルゴリズムとその実現精度のシミュレーション解析結果、垂直降下フェーズにおける誘導能力の概略検討結果などについて示す。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | SELENE(SELenological and ENgineering Explorer)-B is a proposed lunar landing system that performs scientific missions, such as geological surveys using a rover in a specified area on the lunar surface. A high accuracy guidance, navigation and control (GN and C) system is required for this mission and navigation and guidance accuracy at the terminal point of the landing phase is critical. A hybrid navigation system, using the sensors that provide an altitude and position relative to the lunar surface, is required for accuracy and reliability. Furthermore, a new guidance law is proposed that is based on a simple ON-OFF thrust control strategy that can perform accurate powered-descent guidance despite acceleration errors. In the vertical descent phase, the guidance capability for horizontal maneuvers and the position, velocity and attitude control strategy using on-off thrusters are investigated by numerical simulations. This paper summarizes the results of the investigations on the GN and C system of SELENE-B. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0046652024 |