「運動と振動の制御」シンポジウム講演論文集
Online ISSN : 2424-3000
セッションID: B03
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B03 捩り振動を考慮した柔軟宇宙構造物の振動制御(OS10-1 宇宙機と宇宙構造物の制御)
伊藤 賢志渡辺 亨背戸 一登
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This paper deals with the active vibration control with twisting vibration. The control objects are flexible plates like solar array panels supported by a rigid-body rotor like a space station. Two flexible plates are connected with each other through the electromagnetic actuators fixed with the flexible arms. As a vibration control mechanism, the method using the interactive force between structures is applied for vibration control of these plate structures. Then, these structures are expressed by the lumped parameter system "4-DOF model" using the reduced order physical modeling method. To prevent so-called spillover, a second order low-pass filter is built in the control system. The LQ control method is used to obtain feedback gain. Computer simulations showed the effectiveness of presented control method.

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© 2005 一般社団法人 日本機械学会
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