ロケット搭載用太陽センサの飛翔実験および地上における姿勢決定システム

Material type: 文書・図像類

Author: 広川, 英治ほか

Publisher: 宇宙航空研究開発機構

Publication date: 2006-11-01

Material Format: Digital

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Note (General)：: In order to detect attitude for spinning rocket we have developed a sun aspect sensor (RSAS) with a field of view of 128 degree and resolution of 0.5 ...

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Material Type: 文書・図像類
Title: ロケット搭載用太陽センサの飛翔実験および地上における姿勢決定システム
Author/Editor: 広川, 英治
成田, 伸一郎
太刀川, 純孝
森田, 泰弘
Hirokawa, Eiji
Narita, Shinichiro
Tachikawa, Sumitaka
Morita, Yasuhiro
Author Heading: 広川, 英治
成田, 伸一郎
太刀川, 純孝
森田, 泰弘
Hirokawa, Eiji
Narita, Shinichiro
Tachikawa, Sumitaka
Morita, Yasuhiro
Publication, Distribution, etc.: 宇宙航空研究開発機構
Publication Date: 2006-11-01
Publication Date (W3CDTF): 2006-11-01
Alternative Title: Flight test of rocket sun aspect sensor and attitude determination system on the ground by M-V-8 launch
Periodical title: 宇宙航空研究開発機構特別資料: 平成18年度　宇宙航空研究開発機構　総合技術研究本部　宇宙科学研究本部　研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
No. or year of volume/issue: JAXA-SP-06-006
Volume: JAXA-SP-06-006
Pages: 359-362
ISSN (Periodical Title): ISSN : 1349-113X
Text Language Code: jpn
Subject Heading: 太陽センサ
ロケット打上げ
観測ロケット
姿勢制御
環境試験
フォトダイオード
テレメトリ
慣性基準装置
solar sensor
rocket launching
sounding rocket
attitude control
environmental test
photodiode
telemetry
inertial reference unit
Target Audience: 一般
Note (General): In order to detect attitude for spinning rocket we have developed a sun aspect sensor (RSAS) with a field of view of 128 degree and resolution of 0.5 degree. Furthermore, we have developed the attitude determination system using data of sun sensor and geomagnetic aspect sensor on the ground. The sun sensor was flight tested with ISAS rocket (M-V-8) on 23rd February 2006. Purposes of the test were environmental test (vibration shock etc.) during launching. It was found the sun sensor had no trouble during flight and able to determine attitude for spinning rocket.
資料番号: AA0049500076
レポート番号: JAXA-SP-06-006
Source: https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6060&item_no=1&attribute_id=31&file_no=1
https://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=6060&item_no=1&attribute_id=31&file_no=1
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