{"created":"2023-06-20T15:10:04.943498+00:00","id":39675,"links":{},"metadata":{"_buckets":{"deposit":"d56f2f5b-8414-4bf4-b078-5216c8978bdd"},"_deposit":{"created_by":1,"id":"39675","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39675"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039675","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["443833","443830","443832","443831"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Flight simulation program for high altitude long endurance unmanned vehicle"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1995-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"24","bibliographicPageStart":"1","bibliographicVolumeNumber":"688","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"本資料では、高高度無人機の誘導・制御則を評価・検討するために開発した飛行シミュレーションプログラムと、設計した誘導則、ならびに飛行シミュレーション結果について報告する。まず、運動方程式は地球を平面として取り扱い、3次元6自由度と3次元3自由度の運動方程式を導く。ついで、レクテナ翼を有する機体形状について、空力特性と重量特性を推算する。そして、プロペラ特性を風洞試験データに基づき定式化する。最後に高度20kmで遭遇することが予想される風について整理する。以上のような構成要素に基づき、飛行シミュレーションプログラムを開発した。また本資料では、マイクロウエーブ伝送装置を中心としたある限られた範囲内に無人機を閉じ込めておくことを目的として、水平面内の運動のみを考慮した誘導則を提案する。そして、開発した飛行シミュレーションプログラムを用いて、本資料で提案する誘導則による飛行シミュレーションを行った。得られた結果から、比較的強い風に遭遇しても、無人機を限られた空間内に閉じ込めておくことが可能である見通しを得た。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"This paper describes the development process of a flight simulation program for estimation and examination of guidance and control law of a High Altitude Long Endurance Unmanned Vehicle (HALEUV). At first, equations of motion of three degrees of six freedom and three freedom are derived assuming that the earth is a flat plane. Then, the aerodynamic characteristics of HALEUV are estimated. Propeller performance is formulated based on wind tunnel data. The wind data is set at an altitude of 20 km, which HALEUV is expected to encounter. Also, the guidance law for the HALEUV is designed to be closed within a limited area with a microwave transmitter at its center. This law is incorporated into the flight simulation program, and flight simulation is performed. The results indicate that the HALEUV can stay within an area with a radius of 3 km, even if the HALEUV encounters with a strong wind.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000095000","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 TM-688","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":"0452-2982","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":"AN00314334","subitem_source_identifier_type":"NCID"}]},"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 新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Aircraft Research Group"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"鈴木, 広一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"外立, 政隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Hirokazu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hashidate, Masataka","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":"naltm00688.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00688.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39675/files/naltm00688.pdf"},"version_id":"65e55db0-0625-4d4c-8cb4-2fcd1fcad553"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"飛行シミュレーションプログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"誘導則","subitem_subject_scheme":"Other"},{"subitem_subject":"高高度無人機","subitem_subject_scheme":"Other"},{"subitem_subject":"HALEUV","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"レクテナ翼","subitem_subject_scheme":"Other"},{"subitem_subject":"マイクロ波伝送装置","subitem_subject_scheme":"Other"},{"subitem_subject":"運動方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"横方向姿勢運動","subitem_subject_scheme":"Other"},{"subitem_subject":"風荷重","subitem_subject_scheme":"Other"},{"subitem_subject":"空間内閉込め","subitem_subject_scheme":"Other"},{"subitem_subject":"航続時間","subitem_subject_scheme":"Other"},{"subitem_subject":"プロペラ機","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"guidance law","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high altitude long endurance unmanned vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HALEUV","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"rectilinear wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"microwave power transmission","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"motion equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transverse direction attitude motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind load","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spatial area stay","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"long endurance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"propeller aircraft","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":"高高度無人機の飛行シミュレーションプログラム","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"高高度無人機の飛行シミュレーションプログラム"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"39675","relation_version_is_last":true,"title":["高高度無人機の飛行シミュレーションプログラム"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:53.697532+00:00"}