{"created":"2023-06-20T14:40:36.540657+00:00","id":7524,"links":{},"metadata":{"_buckets":{"deposit":"a8000c92-1866-4365-bd70-9dd78599ca3a"},"_deposit":{"created_by":1,"id":"7524","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7524"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007524","sets":["1543:1544:1557","1887:1891"]},"author_link":["40152","40150","40149","40151"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"インターセプタを用いた小天体フライバイのための統合型航法誘導制御"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"132","bibliographicPageStart":"127","bibliographic_titles":[{"bibliographic_title":"第16回アストロダイナミクスシンポジウム講演後刷り集　2006"},{"bibliographic_title":"Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"ISAS/JAXAでは超小型探査機「インターセプタ」を用いた小天体のフライバイミッションを計画している。本計画は「のぞみ(PLANET-B: Mars Orbiter)」のフライバイと異なり、積極的に近接点を通過することで多様な観測を行うことを目指している。一般に弾道飛行の場合、光学観測のみの情報ではフライバイ時の相対軌道決定は不可能である。そこで地上観測によって目的天体との相対速度ベクトル情報を取得することを前提とし、光学航法と電波航法を統合した航法を提案する。このための制御則を数値シミュレーションにより導出し、地上実験によって検証する。地上実験では、小石に光を当ててカメラで撮像したデータを用いてロボットシミュレータを目標軌道に誘導する。本論文では、これらの結果を報告する。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Institute of Space and Astronautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA) is currently planning the missions that the small probe 'interceptor' flybys near-Earth objects. Interceptor is very small probe. An interceptor observes spectrum, takes close images, and determines mass of a NEO (Near Earth Object) during a flyby. The weight of interceptor is less than 10 kg. This paper shows three types of missions. In general, it is impossible to determine the relative orbit during flyby only with optical information. Thus the optical navigation needs to be combined with the radio navigation that should provide the relative velocity vector information. In this paper, the integrated guidance and navigation strategy of interceptor is proposed.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063481023","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構 宇宙科学研究本部"},{"subitem_text_value":"トヨタ自動車"}]},"item_5_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 Space and Astronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Toyota Motor Corporation"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"森, 治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"多羅尾, 康太"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Mori, Osamu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tarao, Kota","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"衛星誘導","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙航行","subitem_subject_scheme":"Other"},{"subitem_subject":"無線航法","subitem_subject_scheme":"Other"},{"subitem_subject":"光学航法","subitem_subject_scheme":"Other"},{"subitem_subject":"誤差分析","subitem_subject_scheme":"Other"},{"subitem_subject":"フライバイミッション","subitem_subject_scheme":"Other"},{"subitem_subject":"ハイブリッド航法システム","subitem_subject_scheme":"Other"},{"subitem_subject":"小型衛星技術","subitem_subject_scheme":"Other"},{"subitem_subject":"画像処理","subitem_subject_scheme":"Other"},{"subitem_subject":"制御理論","subitem_subject_scheme":"Other"},{"subitem_subject":"計算機シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"ロボットシミュレータ","subitem_subject_scheme":"Other"},{"subitem_subject":"RS","subitem_subject_scheme":"Other"},{"subitem_subject":"インターセプタ","subitem_subject_scheme":"Other"},{"subitem_subject":"satellite guidance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"radio navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"optical navigation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"error analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flyby mission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hybrid navigation system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"small satellite technology","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"image processing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computerized simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"robotics simulator","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"interceptor","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Integrated guidance, navigation and control in flying-by small bodies using interceptor","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Integrated guidance, navigation and control in flying-by small bodies using interceptor","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1557","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7524","relation_version_is_last":true,"title":["Integrated guidance, navigation and control in flying-by small bodies using interceptor"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:38:11.329517+00:00"}