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Analysis of friction effects on satellite antenna driving mechanism with clearance joints

机译:间隙接头对卫星天线驱动机构的摩擦影响分析

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The existence of clearance in joints of mechanism is inevitable. In this paper, the friction effects in clearance joints on dynamic responses of driving mechanism of satellite antenna are studied. Considering clearances in joints, the contact force model in clearance joints is established using a nonlinear continuous contact force model and the friction effect is considered by using a modified Coulomb friction model. Then the dual-axis driving mechanism of satellite antenna with clearance joints is used as the application example. The numerical simulation of dual-axis driving mechanism with clearance joints is presented. The friction effects of clearance joint on dynamic responses of the dual-axis driving mechanism are discussed and analyzed quantitatively for four cases with different friction coefficients. The investigation results show that the increase of friction coefficient will decrease the vibration amplitude of the driving mechanism system.
机译:机构关节中存在间隙是不可避免的。本文研究了间隙接头的摩擦效应对卫星天线驱动机构动力响应的影响。考虑关节间隙,使用非线性连续接触力模型建立间隙关节的接触力模型,并使用改进的库仑摩擦模型考虑摩擦效果。然后以带间隙接头的卫星天线双轴驱动机构为应用实例。提出了带有间隙关节的双轴驱动机构的数值模拟。对四种摩擦系数不同的情况,间隙间隙对双轴驱动机构动力响应的摩擦效应进行了讨论和定量分析。研究结果表明,摩擦系数的增加将减小驱动机构系统的振动幅度。

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