ETS-8軌道上実験の検討:誘導制御技術の研究

Material type: 文書・図像類

Author: 山本, 昌幸ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-01-20

Material Format: Digital

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Note (General)：: This report describes the studies on the on-orbit system identification and attitude control experiments using ETS-8 (Engineering Test Satellite-8). E...

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Material Type: 文書・図像類
Title: ETS-8軌道上実験の検討:誘導制御技術の研究
Author/Editor: 山本, 昌幸
巳谷, 真司
大谷, 崇
山口, 功
葛西, 時雄
井川, 寛隆
濱田, 吉郎
池田, 正文
臼井, 基文
砂川, 圭
Yamamoto, Masayuki
Mitani, Shinji
Otani, Takashi
Yamaguchi, Isao
Kasai, Tokio
Igawa, Hirotaka
Hamada, Yoshiro
Ikeda, Masafumi
Usui, Motofumi
Sunagawa, Kei
Author Heading: 山本, 昌幸
巳谷, 真司
大谷, 崇
山口, 功
葛西, 時雄
井川, 寛隆
濱田, 吉郎
池田, 正文
臼井, 基文
砂川, 圭
Yamamoto, Masayuki
Mitani, Shinji
Otani, Takashi
Yamaguchi, Isao
Kasai, Tokio
Igawa, Hirotaka
Hamada, Yoshiro
Ikeda, Masafumi
Usui, Motofumi
Sunagawa, Kei
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-01-20
Publication Date (W3CDTF): 2006-01-20
Alternative Title: On-orbit experiments using ETS-8: Study on guidance and control technology
Periodical title: 宇宙航空研究開発機構特別資料: 平成16年度総合技術研究本部宇宙領域宇宙科学研究本部合同研究成果報告書:人工衛星系基盤技術 = JAXA Special Publication: FY2004 Report of Joint Research Achievements of the Space Division of Institute of Aerospace Technology and Institute of Space and Astronautical Science: Basic Technologies of Satellite Systems
No. or year of volume/issue: JAXA-SP-05-008
Volume: JAXA-SP-05-008
Pages: 247-252
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 大型宇宙構造物
大型展開リフレクタ
ETS-8
H-2A打上げ機
太陽電池アレイ
軌道上宇宙試験
宇宙技術実験
衛星姿勢制御
リフレクタアンテナ
large space structure
large deployable reflector
H-2A launch vehicle
solar array
orbital space test
space technology experiment
satellite attitude control
reflector antenna
Target Audience: 一般
Note (General): This report describes the studies on the on-orbit system identification and attitude control experiments using ETS-8 (Engineering Test Satellite-8). ETS-8 will be launched by H-2A launch vehicle in fiscal year 2006. ETS-8 has large-scale, flexible structure like Large Deployable Reflector or Solar Array Paddle. Using the result of the on-orbit system identification experiments, we can evaluate the on-orbit flexible characteristic and contribute to the control system design for the next flexible satellite. We aim at the establishment of the robust attitude control technology for flexible satellites through these attitude control experiments.
資料番号: AA0049054050
レポート番号: JAXA-SP-05-008
Access Restrictions: 限定公開
Periodical Title (NCID): AA11984031
https://ci.nii.ac.jp/ncid/AA11984031
Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）
https://irdb.nii.ac.jp
Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ