{"created":"2023-06-20T14:35:59.566523+00:00","id":2286,"links":{},"metadata":{"_buckets":{"deposit":"a92c6d2b-c119-40b8-8840-402efb88c68a"},"_deposit":{"created_by":1,"id":"2286","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"2286"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00002286","sets":["1887:1893","9:10:256:296"]},"author_link":["4951","4953","4948","4957","4963","4960","4956","4964","4949","4955","4952","4965","4961","4962","4950","4959","4958","4954"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-12-28","bibliographicIssueDateType":"Issued"},"bibliographicVolumeNumber":"JAXA-RR-05-013E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構研究開発報告"},{"bibliographic_title":"JAXA Research and Development Report","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本論文は、月面精密着陸に必要な誘導制御則について論ずる。取り扱う月面軟着陸機は、以前提案されていたSELENE-B(月軟着陸実験計画)と同じ構成を持つと仮定する。着陸機は、岩石や小さなクレータなどの危険な場所を避けつつ、科学的に意義のある地点へ精密に着陸することが要求される。本稿では、これを満足する着陸誘導制御則を設計し、モンテカルロシミュレーションによって評価を行なう。SELENE-Bと同じ構成および着陸シーケンスでは、安全かつ精密な着陸は難しいことをシミュレーションで示し、その結果を受けて構成などに変更を加え、更なるシミュレーションで精密着陸の成立性を検証する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper concerns the evaluation of a guidance and control system for lunar landing. The lander, which is supposed to have the same configuration of SELENE-B (SELenological and ENgineering Explorer-B), is required to land precisely at a site where there are scientifically important features, with minimal fuel consumption while avoiding surface obstacles such as rocks and small craters which might jeopardize the landing. The guidance and control system are designed for this aim, and the feasibility of the landing is tested by Monte Carlo simulation. The results, however, indicated that the original configuration and landing sequence are not appropriate for precise and safe landing. Therefore, based on the results, the configuration and landing sequence are modified and tested by Monte Carlo simulation again.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0049192000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-RR-05-013E","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-1113","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA1192675X","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"宇宙航空研究開発機構 総合技術研究本部"},{"subitem_text_value":"横浜国立大学"},{"subitem_text_value":"三菱スペース・ソフトウエア"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Institute of Aerospace Technology"},{"subitem_text_language":"en","subitem_text_value":"Yokohama National University"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software Co. Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"濱田, 吉郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"二宮, 哲次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"片山, 保宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"四宮, 康雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松本, 甲太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山本, 真行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"澤井, 秀次郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上野, 誠也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"林, 健太郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamada, Yoshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Tetsujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katayama, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shinomiya, Yasuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsumoto, Kotaro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamamoto, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sawai, Shujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueno, Seiya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hayashi, Kentaro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-15"}],"displaytype":"detail","filename":"49192000.pdf","filesize":[{"value":"2.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"49192000.pdf","url":"https://jaxa.repo.nii.ac.jp/record/2286/files/49192000.pdf"},"version_id":"5112b1f9-aef7-4d39-b283-046f33e93dbc"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星誘導","subitem_subject_scheme":"Other"},{"subitem_subject":"衛星制御","subitem_subject_scheme":"Other"},{"subitem_subject":"月面着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"月面着陸機","subitem_subject_scheme":"Other"},{"subitem_subject":"SELENE-B","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸シーケンス","subitem_subject_scheme":"Other"},{"subitem_subject":"基準軌道","subitem_subject_scheme":"Other"},{"subitem_subject":"着陸シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"モンテカルロ法","subitem_subject_scheme":"Other"},{"subitem_subject":"障害物回避","subitem_subject_scheme":"Other"},{"subitem_subject":"位置誤差","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite guidance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar landing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar lander","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"SELENE-B","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing sequence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reference trajectory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"landing simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Monte Carlo method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"obstacle avoidance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"position error","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Feasibility study for precise lunar landing using SELENE-B lander configuration","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Feasibility study for precise lunar landing using SELENE-B lander configuration","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["296","1893"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"2286","relation_version_is_last":true,"title":["Feasibility study for precise lunar landing using SELENE-B lander configuration"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T09:25:16.088532+00:00"}