球面空気軸受支持模擬衛星の慣性主軸決定法

Material type: 文書・図像類

Author: 村上, 力ほか

Publisher: 航空宇宙技術研究所

Publication date: 1976-04

Material Format: Digital

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Note (General)：: A new method of determination of three principal axes of inertia of a simulated satellite which is supported on a spherical air bearing is described.O...

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Material Type: 文書・図像類
Title: 球面空気軸受支持模擬衛星の慣性主軸決定法
Author/Editor: 村上, 力
木田, 隆
中島, 厚
MURAKAMI, Chikara
KIDA, Takashi
NAKAJIMA, Atsushi
Author Heading: 村上, 力
木田, 隆
中島, 厚
MURAKAMI, Chikara
KIDA, Takashi
NAKAJIMA, Atsushi
Publication, Distribution, etc.: 航空宇宙技術研究所
Publication Date: 1976-04
Publication Date (W3CDTF): 1976-04
Alternative Title: A Method of Determination of Three Principal Axes of Inertia of A Simulated Satellite Supported on A Spherical Air Bearing
Periodical title: 航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-450
No. or year of volume/issue: 450
Volume: 450
Pages: 13-
ISSN (Periodical Title): ISSN : 0389-4010
Text Language Code: jpn
Target Audience: 一般
Note (General): A new method of determination of three principal axes of inertia of a simulated satellite which is supported on a spherical air bearing is described.One axis is determined by observation of the wobbling motion of a simulated spinning satellite.The remaining axes are determined by envelopes of Lissajous’ figures obtained from the pendulum oscillation of the satellite which has small mass appendages.The validity of this method is confirmed experimeny.
資料番号: NALTR0450000
レポート番号: NAL TR-450
Access Restrictions: 限定公開
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