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Servo system design of direct-drive aerospace linear electro-mechanical actuator

机译:直驱航天线性机电执行器伺服系统设计

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According to the high accuracy, broad band and large load demanding for the actuator which put forward by the spacecraft, servo system of direct drive linear electro-mechanical actuator is designed. In order to improve precision and dynamic property of the servo system, direct-drive torque motor combined ball screws are used and high precision optical absolute encoder are used for feedback. SimPowerSystems toolbox is adopted to set up model and simulation which can observe the servo system operation state directly on the basis of close loop servo system math model in order to improve the accuracy of servo system model. Simulation and experimental results show that direct drive linear electro-mechanical actuator with a good ability of servo movement. In the case of load 20Kg, amplitude attenuation in 1 dB, bandwidth lag 10°, dynamic response is no less than 12Hz and absolute position accuracy is no more than 0.2mm. It can satisfy the servo system requirements of high accuracy, broad band and large load.
机译:针对航天器对致动器的高精度,高带宽,高负荷的要求,设计了直驱式线性机电致动器的伺服系统。为了提高伺服系统的精度和动态性能,使用了直接驱动扭矩电机组合滚珠丝杠,并使用了高精度光学绝对编码器进行反馈。采用SimPowerSystems工具箱进行建模和仿真,可以在闭环伺服系统数学模型的基础上直接观察伺服系统的运行状态,以提高伺服系统模型的精度。仿真和实验结果表明,直接驱动线性机电致动器具有良好的伺服运动能力。在负载为20Kg的情况下,幅度衰减为1 dB,带宽滞后为10°,动态响应不小于12Hz,绝对位置精度不大于0.2mm。它可以满足高精度,宽带和大负载的伺服系统要求。

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