{"created":"2023-06-20T15:07:28.675304+00:00","id":36848,"links":{},"metadata":{"_buckets":{"deposit":"50290a7d-d27e-4e03-a318-57a673253837"},"_deposit":{"created_by":1,"id":"36848","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36848"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036848","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["477861","477862","477860","477859"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of flight control system and estimation of stability and control derivatives"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-09","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"87","bibliographicPageStart":"78","bibliographicVolumeNumber":"32","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"24-25 Jul. 1996","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"極超音速飛行実験機(HYFLEX)は、ほぼ計画通りに再突入飛行を行ったが、その成功は誘導制御系の働きに負うところが大きい。本論文では、制御則の概要を述べるとともに、実飛行をシミュレーションと比較することにより姿勢制御の評価を行う。飛行データは、制御則が十分な安定性・制御性を与えたことを示している。さらに、制御系設計に用いられた機体モデルの妥当性を評価するために、安定微係数の推定値と予測値を比較する。安定微係数の推定値は最尤法によって得られたものである。その結果、飛行データから推定された微係数は、少数の例外を除いて概ね予測値に一致していることが分かった。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The HYFLEX (Hypersonic Flight Experiment) vehicle successfully performed a gliding reentry flight. The success of the flight depended entirely on an on-board flight control system, because the experimental aircraft was an unmanned, control configured vehicle. This paper summarizes the control laws and shows the results of the actual flight in comparison with a simulated flight. The flight data show that the control laws provided enough stability and control performance. The stability and control derivative estimates are also presented to assess the validity of the design model. The derivatives were obtained using a maximum likelihood estimation program. The flight results agreed with predictions fairly well except a few derivatives.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000584010","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-32","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石本, 真二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐々, 修一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishimoto, Shinji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sasa, Shuichi","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0032010.pdf","filesize":[{"value":"704.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0032010.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36848/files/nalsp0032010.pdf"},"version_id":"52a16789-90bc-4c32-85f5-43899d41a204"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速飛行実験","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"安定性解析","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_scheme":"Other"},{"subitem_subject":"リアクションコントロールシステム","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"可制御性","subitem_subject_scheme":"Other"},{"subitem_subject":"最尤法","subitem_subject_scheme":"Other"},{"subitem_subject":"安定微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"反力制御システム","subitem_subject_scheme":"Other"},{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"パラメータ推定","subitem_subject_scheme":"Other"},{"subitem_subject":"空力微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HYFLEX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"RCS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"controllability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"maximum likelihood estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stability derivative","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reaction control system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parameter estimation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic control derivative","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"姿勢制御の評価と空力微係数の推算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"姿勢制御の評価と空力微係数の推算"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"36848","relation_version_is_last":true,"title":["姿勢制御の評価と空力微係数の推算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:30:43.842313+00:00"}