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Redesign and the flight result of the M-V-5 ING
https://jaxa.repo.nii.ac.jp/records/7754
https://jaxa.repo.nii.ac.jp/records/77543e2f572a-e583-46bb-9d79-0fb581b55e22
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Redesign and the flight result of the M-V-5 ING | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 慣性誘導 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | M-5シリーズ打上げ機 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 姿勢制御 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アルゴリズム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アンテナ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | FOG | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 周波数応答 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | フィードバック制御 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | inertial navigation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | M-5 series launch vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | attitude control | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | algorithm | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | antenna | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | FOG | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | frequency response | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | feedback control | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル | ||||||
その他のタイトル | M-V-5 INGの改良点と飛翔結果 | |||||
著者 |
斉藤, 一晶
× 斉藤, 一晶× 後藤, 晋一× 江西, 達也× Saito, Kazuaki× Goto, Shinichi× Enishi, Tatsuya |
|||||
著者所属 | ||||||
三菱プレシジョン | ||||||
著者所属 | ||||||
三菱プレシジョン | ||||||
著者所属 | ||||||
三菱プレシジョン | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Precision Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Precision Co. Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Precision Co. Ltd. | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS) | |||||
書誌情報 |
平成15年度アストロダイナミクスシンポジウム:講演後刷り集 en : ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers p. 329-332, 発行日 2004-02 |
|||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | M-5型ロケットに搭載されるING(Inertial Navigation and Guidance)は、ロケットの姿勢制御を主な機能としている。M-5号機では、INGを含め様々な改良が行われた。ここでは、INGの姿勢制御の基礎となる角速度センサ(FOG)の振動下での性能の改善について述べる。 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Inertial Navigation and Guidance (ING) subsystems are boarded on the M-5 series launch vehicle mainly for attitude control. The ING for the M-5 was improved some functionality and performance. The major points are: 1) Modify the control algorithm for the new M25, the 2nd stage rocket motor, 2) Implement selection logic for the optimum transmission antennas by the roll angle, 3) Reduce angular drifts under vibration, and 4) Modify control algorithm for the blow-down type Side Jets (SJ). This paper provides improvement of Fiber Optic Gyro (FOG) to reduce angular drifts under vibration. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0918-8053 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0046652053 |