年次大会
Online ISSN : 2424-2667
ISSN-L : 2424-2667
セッションID: S192016
会議情報
S192016 小型CMGシステム駆動開始・終了時における衛星姿勢制御手法の提案と検証
神谷 崇志松永 三郎
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会議録・要旨集 フリー

詳細
抄録
"TSUBAME", an earth and astronomical observation technology demonstration satellite being now developed by Matunaga laboratory at ISAS/JAXA, has the control moment gyro (CMG) system arranged in the pyramid type as an attitude control device. In this paper, we firstly mention the influence of disturbance torque which the CMG system generates at activation and deactivation on the satellite attitude, and propose an attitude stabilization control method, and explain numerical simulation results of the proposal method compared with hardware experimental results.
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© 2012 一般社団法人 日本機械学会
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