@inproceedings{oai:jaxa.repo.nii.ac.jp:00007754,
 author = {斉藤, 一晶 and 後藤, 晋一 and 江西, 達也 and Saito, Kazuaki and Goto, Shinichi and Enishi, Tatsuya},
 book = {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, ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers},
 month = {Feb},
 note = {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。, 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., 資料番号: AA0046652053},
 pages = {329--332},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {Redesign and the flight result of the M-V-5 ING},
 year = {2004}
}