{"_buckets": {"deposit": "bb206f9a-70fa-4e87-97db-8e0b2196a093"}, "_deposit": {"created_by": 1, "id": "8135", "owners": [1], "pid": {"revision_id": 0, "type": "depid", "value": "8135"}, "status": "published"}, "_oai": {"id": "oai:jaxa.repo.nii.ac.jp:00008135", "sets": ["1578", "1891"]}, "author_link": ["44972", "44969", "44970", "44973", "44968", "44971"], "item_5_alternative_title_2": {"attribute_name": "その他のタイトル（英）", "attribute_value_mlt": [{"subitem_alternative_title": "Considerations about the disturbance and the construction way of a space solar power system with gravity-gradient stabilization"}]}, "item_5_biblio_info_10": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2004-06", "bibliographicIssueDateType": "Issued"}, "bibliographicPageEnd": "93", "bibliographicPageStart": "89", "bibliographic_titles": [{"bibliographic_title": "第23回宇宙エネルギーシンポジウム　平成15年度"}, {"bibliographic_title": "The 23rd ISAS Space Energy Symposium March 9, 2004", "bibliographic_titleLang": "en"}]}]}, "item_5_description_17": {"attribute_name": "抄録（英）", "attribute_value_mlt": [{"subitem_description": "A SPS (Solar Power Satellite) which is a part of the Space Solar System (SSPS) project has been studied at the USEF. Quasi-static analysis had been carried out for the practical SPS. The present purpose is to evaluate the attitude stability of the SPS under construction. During construction, it is assumed that the modules of 100 x 95 sq m are arranged in the shape of line. As the result of quasi-static analysis, it is shown that the roll and yaw angular frequencies of attitude motion are twice and once as large as orbital angular velocity in first step of the construction, respectively. Furthermore, as the result of dynamical analysis, amplitudes of the roll and yaw angles tend to divergence in first step. To avoid such a divergence, another model was proposed which is constructed keeping similar configuration. The construction way is called construction with similarity. From the result of simulations, it is shown that divergences in the roll and yaw angles can be avoided in the construction with similarity. However, the stability around the pitch and yaw axes are weak in first step for construction with similarity. In particular, maximum amplitude around the pitch axis is 5 deg. Therefore, both constructions need active attitude control because there are problems in first step of the constructions.", "subitem_description_type": "Other"}]}, "item_5_description_32": {"attribute_name": "資料番号", "attribute_value_mlt": [{"subitem_description": "資料番号: AA0047275019", "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_20": {"attribute_name": "その他キーワード", "attribute_value_mlt": [{"subitem_text_value": "宇宙船設計、試験及び性能"}]}, "item_5_text_35": {"attribute_name": "JAXAカテゴリ", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ: シンポジウム・研究会"}]}, "item_5_text_36": {"attribute_name": "JAXAカテゴリ2", "attribute_value_mlt": [{"subitem_text_value": "JAXAカテゴリ2: IS"}]}, "item_5_text_42": {"attribute_name": "シンポジウム区分", "attribute_value_mlt": [{"subitem_text_value": "シンポジウム区分: 002"}]}, "item_5_text_43": {"attribute_name": "DSpaceコレクション番号", "attribute_value_mlt": [{"subitem_text_value": "DSpaceコレクション番号: 7"}]}, "item_5_text_6": {"attribute_name": "著者所属", "attribute_value_mlt": [{"subitem_text_value": "北海道大学 大学院工学研究科"}, {"subitem_text_value": "北海道大学 大学院工学研究科"}, {"subitem_text_value": "宇宙航空研究開発機構 宇宙科学研究本部"}]}, "item_5_text_7": {"attribute_name": "著者所属（英）", "attribute_value_mlt": [{"subitem_text_language": "en", "subitem_text_value": "Hokkaido University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Hokkaido University Graduate School of Engineering"}, {"subitem_text_language": "en", "subitem_text_value": "Japan Aerospace Exploration Agency Institute of Space and Astronautical Science"}]}, "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": "高井, 伸明"}], "nameIdentifiers": [{"nameIdentifier": "44968", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "石村, 康生"}], "nameIdentifiers": [{"nameIdentifier": "44969", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "佐々木, 進"}], "nameIdentifiers": [{"nameIdentifier": "44970", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Takai, Nobuaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44971", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Ishimura, Kosei", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44972", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "Sasaki, Susumu", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "44973", "nameIdentifierScheme": "WEKO"}]}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "太陽発電衛星", "subitem_subject_scheme": "Other"}, {"subitem_subject": "重力勾配安定化", "subitem_subject_scheme": "Other"}, {"subitem_subject": "宇宙機安定性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "動的安定性", "subitem_subject_scheme": "Other"}, {"subitem_subject": "共鳴周波数", "subitem_subject_scheme": "Other"}, {"subitem_subject": "衛星設計", "subitem_subject_scheme": "Other"}, {"subitem_subject": "慣性モーメント", "subitem_subject_scheme": "Other"}, {"subitem_subject": "組立て", "subitem_subject_scheme": "Other"}, {"subitem_subject": "solar power satellite", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "gravity-gradient stabilization", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "spacecraft stability", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "dynamic stability", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "resonant frequency", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "satellite design", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "moment of inertia", "subitem_subject_language": "en", "subitem_subject_scheme": "Other"}, {"subitem_subject": "assembling", "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": "重力傾斜安定型太陽発電衛星の外乱評価とその組み立てに関する考察", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "重力傾斜安定型太陽発電衛星の外乱評価とその組み立てに関する考察"}]}, "item_type_id": "5", "owner": "1", "path": ["1578", "1891"], "permalink_uri": "https://jaxa.repo.nii.ac.jp/records/8135", "pubdate": {"attribute_name": "公開日", "attribute_value": "2015-03-26"}, "publish_date": "2015-03-26", "publish_status": "0", "recid": "8135", "relation": {}, "relation_version_is_last": true, "title": ["重力傾斜安定型太陽発電衛星の外乱評価とその組み立てに関する考察"], "weko_shared_id": -1}