人工衛星の高性能姿勢制御の研究

Material type: 文書・図像類

Author: 遠藤, 達也ほか

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 is the report of a study of high performance maneuver for artificial satellite. Especially, CMG (Control Moment Gyro) aiming to agile reorientati...

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Material Type: 文書・図像類
Title: 人工衛星の高性能姿勢制御の研究
Author/Editor: 遠藤, 達也
川井, 洋志
関口, 毅
鈴木, 秀人
Endo, Tatsuya
Kawai, Hiroshi
Sekiguchi, Takeshi
Suzuki, Hideto
Author Heading: 遠藤, 達也
川井, 洋志
関口, 毅
鈴木, 秀人
Endo, Tatsuya
Kawai, Hiroshi
Sekiguchi, Takeshi
Suzuki, Hideto
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: A study of high performance maneuver for artificial satellite
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: 219-224
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: コントロールモーメントジャイロ
衛星姿勢制御
宇宙機マヌーバ
角運動量
慣性モーメント
bang-bang制御
トルク
リアクションホイール
アクチュエータ
control moment gyroscope
satellite attitude control
spacecraft maneuver
angular momentum
moment of inertia
bang-bang control
torque
reaction wheel
actuator
Target Audience: 一般
Note (General): This is the report of a study of high performance maneuver for artificial satellite. Especially, CMG (Control Moment Gyro) aiming to agile reorientation maneuver is discussed in this report. The number and the arrangement of the CMG cluster were examined, for Rest-to-Rest maneuvering. The performance presumption parameter to the first design estimate was derived. The CMG assembly design for agile maneuver is determined by requirement of angular momentum and the moment of inertia of satellite. The result of the CMG assembly arrangement should be discussed from the point of electrical energy consumption, precise weight estimation and cost.
資料番号: AA0049054045
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