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

机译:基于脐带连接的无干扰有效载荷的指向精度和指向稳定性

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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重力波探测航天器中起着重要作用。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动力学模型,指向精度和稳定性分析。提出了一种有效载荷脐带航天器的精确模型,该模型考虑了平移刚度和阻尼效应以及扭转刚度效应。拉格朗日方法用于导出刚柔耦合动力学模型。进行了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,在0.01 Hz至1 Hz的低频下,脐带显着降低了有效载荷的隔振性能。还模拟了另外两种情况,即仅考虑平移刚度效应的不带脐带的有效载荷和带脐带的有效载荷。这三种情况的结果表明,脐带缆大大降低了有效载荷的指向精度,并降低了指向稳定性。扭转刚度对有效载荷的指向精度也有轻微影响。

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