{"created":"2023-06-20T15:11:45.661640+00:00","id":41487,"links":{},"metadata":{"_buckets":{"deposit":"064c990e-c3f9-4774-a29f-04166bf5eceb"},"_deposit":{"created_by":1,"id":"41487","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41487"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041487","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["452651","452653","452655","452657","452659","452656","452658","452652","452654","452650","452648","452649"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"A study on the SELENE model-following control system using the flying test bed"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"13","bibliographicPageStart":"1","bibliographicVolumeNumber":"1418","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"月探査周回衛星(SELENE:SELenological and ENgineering Explorer)プロジェクトでは、2003年に衛星を打ち上げ月周回軌道到達1年後(2004年)に月面への軟着陸を行なう予定である。実際の月面軟着陸に先立つ試験のために、ジェットエンジンを用いた地上飛行試験装置(FTB:Flying Test Bed)が開発され、1999年度末にはその単体飛行試験が行なわれた。今後はSELENEに搭載されるセンサ系・制御系などの、軟着陸モジュール各構成要素の、FTBによる機能確認試験が予定されている。月面軟着陸時の各要素の機能を評価するためには、FTBにSELENEの軟着陸時の動特性を摸擬させた上で、SELENEの各構成要素をFTBに搭載して試験を行なうことが望ましい。そこで本研究では、FTBを用いてSELENEの動特性を摸擬する制御系の検討を行なう。FTB本体の飛行制御系の制御アルゴリスムを改修することで、FTBの状態変数をSELENE月面軟着陸時の状態量に追従させる制御系が実現できることを示す。シミュレーションを行ない、本方式による動特性模擬の有効性を確認した。またSELENEの飛行制御アルゴリズムを検証するために予定されている、FTBにSELENEの制御系を搭戦して飛行を行なう閉ループ総合試験についても、本方式を用いた場合のシミュレーションを行なった。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The SELENE (SELenological and ENgineering Explorer) mission is scheduled for launch in 2003 and will make a soft-landing on the lunar surface in 2004, a year after reaching an orbit around the moon. The Flying Test Bed (FTB) was developed for preliminary terrestrial landing experiments, and the first flight experiment completed at the end of 1999FY. The aim of this experiment was validation of the FTB flight system as a whole. Other experiments are planned to validate the effectiveness of SELENE onboard hardware, such as sensor systems, and software for control systems. In order to test these systems, the FTB should have the same dynamic characteristics as the SELENE. In this paper it is concerned with the controller of the FTB, which enables the FTB to follow the SELENE model. Some simulations are provided to show the effectiveness of the proposed system to follow the SELENE model. A dynamical closed loop test designed to validate the SELENE onboard attitude and orbit control system is also simulated using this system.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028663000","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: NAL TR-1418","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所 飛行システム総合研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 飛行システム総合研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 構造研究部"},{"subitem_text_value":"航空宇宙技術研究所 飛行システム総合研究グループ"},{"subitem_text_value":"宇宙開発事業団"},{"subitem_text_value":"富士重工業"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Systems Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Systems Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structures Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Systems Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Space Development Agency of Japan"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries 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":"山口, 功"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐々, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"板垣, 春昭"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河野, 充"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hamada, Yoshiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ninomiya, Tetsujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamaguchi, Isao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sasa, Shuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Itagaki, Haruaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kono, Mitsuru","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr0001418.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001418.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41487/files/naltr0001418.pdf"},"version_id":"5993384e-58c4-4b3a-b509-858a75583c60"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SELENE","subitem_subject_scheme":"Other"},{"subitem_subject":"月探査周回衛星","subitem_subject_scheme":"Other"},{"subitem_subject":"FTB","subitem_subject_scheme":"Other"},{"subitem_subject":"地上飛行試験装置","subitem_subject_scheme":"Other"},{"subitem_subject":"月面軟着陸","subitem_subject_scheme":"Other"},{"subitem_subject":"地上着陸実験","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢軌道制御系","subitem_subject_scheme":"Other"},{"subitem_subject":"搭載ハードウエア","subitem_subject_scheme":"Other"},{"subitem_subject":"制御システムソフトウエア","subitem_subject_scheme":"Other"},{"subitem_subject":"制御アルゴリズム","subitem_subject_scheme":"Other"},{"subitem_subject":"動的閉ループ試験","subitem_subject_scheme":"Other"},{"subitem_subject":"推進モジュール","subitem_subject_scheme":"Other"},{"subitem_subject":"SELENE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Selenological and engineering explorer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"FTB","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flying test bed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"lunar surface soft landing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"terrestrial landing experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude and orbit control electronics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"onboard hardware","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control system software","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"control algorithm","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dynamic closed loop test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propulsion module","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"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":"SELENEの月着陸時動特性を模擬する地上飛行試験装置の制御系に関する研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"SELENEの月着陸時動特性を模擬する地上飛行試験装置の制御系に関する研究"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41487","relation_version_is_last":true,"title":["SELENEの月着陸時動特性を模擬する地上飛行試験装置の制御系に関する研究"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:10:37.677813+00:00"}