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Active Isolation/Suppression for Satellite Micro-Vibration with Stewart Platform

机译:卫星平台卫星微振动的主动隔离/抑制

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A Stewart platform actuated by voice coil motors (VCM) is selected as the control device to realize active isolation/suppression for micro-vibration onboard a satellite. A single-input-single-output (SISO) control strategy is established for the Stewart platform by decoupling it's dynamic model to the single strut model. The effectiveness of the vibration isolation as well as the limitation on vibration suppression of the Skyhook control method is analyzed, then a positive force feedback (PFF) loop is implemented to achieve isolation. To enhance the robust stability properties of the control system, an acceleration feedback loop is added to the system. Finally, active isolation/suppression experiments are conducted on the Stewart platform's single strut for micro-vibration. A base sweep excitation and a payload side single tone disturbance are induced on the single strut, and isolation/suppression is conducted with this paper's control method. The experimental results show that the control performance is quite good and stable with respect to both vibration isolation and suppression. The effectiveness of the control method is verified and the feasibility of applying this method with the VCM on the Stewart'platform is proved.
机译:选择由音箱电机(VCM)驱动的斯图尔特平台作为控制装置,以实现卫星的微振动的主动隔离/抑制。通过将动态模型解耦到单个Strut模型,为Stewart平台建立了单输入单输出(SISO)控制策略。分析了振动隔离的有效性以及Skyhook控制方法的振动抑制的限制,然后实现了正力反馈(PFF)环以实现隔离。为了增强控制系统的稳定稳定性,将加速反馈回路添加到系统中。最后,主动隔离/抑制实验在Stewart平台的单支质上进行了微振动。在单个支柱上诱导基部扫描激励和有效载荷侧单音干扰,并通过本文的控制方法进行隔离/抑制。实验结果表明,对于振动隔离和抑制,控制性能非常好且稳定。证实了控制方法的有效性,并证明了在Stewart'Platform上使用VCM应用此方法的可行性。

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