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On Pointing Accuracy and Pointing Stability of Disturbance-Free Payload Using Umbilical Connection

机译:用脐带连接指向无干扰有效载荷的准确性和指向稳定性

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Pointing accuracy and pointing stability play an important role in gravitational wave detection spacecraft. This paper presents dynamics model, pointing accuracy and stability analysis of a payload-spacecraft system connected using umbilical and non-contact actuators. Accurate model of payload-umbilical-spacecraft is proposed which takes into account the translational stiffness and damping effects, as well as the torsional stiffness effect. The Lagrangian approach is applied to derive the rigid-flexible coupling dynamics model. Both of the open-loop and closed-loop simulation studies are conducted to investigate the pointing accuracy and stability of the payload. The results indicate that the umbilical significantly degrades the vibration isolation performance of the payload at low frequencies between 0.01 Hz and 1 Hz. Simulation of two other cases, the payload without umbilical and the payload with umbilical considering only the translational stiffness effect, are also performed. The results of these three cases show that the umbilical greatly degrades the pointing accuracy of the payload and lowers the pointing stability. The torsional stiffness also has a slight effect on the pointing accuracy of the payload.
机译:指向精度和指向稳定性在引力波检测航天器中起重要作用。本文介绍了使用脐带和非接触式执行器连接的有效载荷 - 航天器系统的准确性和稳定性分析。提出了准确的有效载荷模型,以考虑到平移刚度和阻尼效应,以及扭转刚度效应。拉格朗日方法应用于导出刚性柔性耦合动力学模型。进行了两个开环和闭环仿真研究,以研究有效载荷的指向精度和稳定性。结果表明,脐带显着降低了0.01Hz和1 Hz之间的低频下有效载荷的振动隔离性能。还执行了另外两个情况的仿真,没有脐带的有效载荷,并且仅考虑平移刚度效果的脐带。这三个案例的结果表明,脐带大大降低了有效载荷的指向精度,并降低了指向稳定性。扭转刚度也对有效载荷的指向精度产生轻微影响。

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