{"created":"2023-06-20T14:40:43.676464+00:00","id":7650,"links":{},"metadata":{"_buckets":{"deposit":"05e82840-f42f-45fc-8b3e-6c956158b78c"},"_deposit":{"created_by":1,"id":"7650","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"7650"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00007650","sets":["1543:1544:1559","1887:1891"]},"author_link":["40992","40991"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"コーニング効果を考慮した姿勢制御の一考察"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"98","bibliographicPageStart":"93","bibliographic_titles":[{"bibliographic_title":"平成16年度アストロダイナミクスシンポジウム:講演後刷り集"},{"bibliographic_title":"ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"非ホロノミックなシステムを用いると、入力としての状態量より多くの状態量を制御することができる。これを上手く利用すれば、機器を少なくすることができ、宇宙機のコストを下げることになる。これが非ホロノミックシステムを制御することの利点である。この論文では、猫ひねりと呼ばれる非ホロノミックな運動をヒントにした新しい姿勢制御方法を提案する。また、この論文では、コーニング効果を使い、猫のひねり運動の検討を行う。コーニング効果とは、ある軸周りに角運動量がゼロであっても、その軸がもとの方向に戻ってきたときに、結果的にその軸周りに回転を生じる現象のことである。コーニング効果によって生じる回転運動は、キネマティクス的である。そして、この研究は、関節を持っている宇宙構造物や宇宙ロボットの姿勢制御に有用であると考える。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Using the nonholonomic system, the number of state quantities, which are controlled, could be more than that of inputs. So, the cost of spacecraft could be small. It is the advantage of control of nonholonomic system. This paper presents a new attitude control method using nonholonomic motion so called as the falling cat phenomenon. This motion is what a cat changes skillfully its attitude during free fall by twisting the body. This paper discusses twisting motion of a falling cat using the coning effect. The coning effect is that even the motion around an axis with no angular momentum results in the residual rotation when it resumes the original orientation. This rotational motion by the coning effect is kinematical. This study is applicable to the attitude control of space structures and space robots having joint.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0047897017","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_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0918-8053","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東海大学 大学院工学研究科"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Tokai University Graduate School of Engineering"}]},"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":"南川, 幸毅"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Minamikawa, Koki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"姿勢制御","subitem_subject_scheme":"Other"},{"subitem_subject":"非ホロノミック運動","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙ロボット","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙構造体","subitem_subject_scheme":"Other"},{"subitem_subject":"捩れ","subitem_subject_scheme":"Other"},{"subitem_subject":"角運動量","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"コーニング効果","subitem_subject_scheme":"Other"},{"subitem_subject":"attitude control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonholonomic motion","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space robot","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"space structure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"twisting","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"angular momentum","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"coning effect","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":"A study of attitude control in consideration of coning effect","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"A study of attitude control in consideration of coning effect","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["1559","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"7650","relation_version_is_last":true,"title":["A study of attitude control in consideration of coning effect"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T07:36:12.427763+00:00"}