Research on High Precision Cryocooler Control System for Satellite-Borne

Li Song, Ziyin Chen, Zhihong Liu, Zhanlei Jin, Rui Cheng, Lanjie Guo
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Abstract

Aiming at meeting the precise temperature requirement (at mK level) of focal-plane in the remote sensing camera, this paper designs a highly accurate temperature control system based on a Pulse tube cryocooler. In order to ameliorate the control precision of temperature, firstly, the design of constant current source circuit is introduced, and the accuracy requirement of the constant current source is given in consideration of the temperature control requirement. Secondly, we devise the circuits for the two-stage amplifier and the filter, and the selection methods of parameters. Finally, the incremental PID control algorithm is introduced, and numerical experimental results of temperature control in vacuum environment are given: (1) The closed-loop accuracy of cryocooler system are given under different temperature control points, and the temperature control accuracy is all within 10mK; (2) When the temperature of the hot plate of cryocooler system changes within 5 °C, the cryocooler system reaches stability again, and the steady-state error is still within 10mK. Therefore, Experimental results indicate that the closed-loop control accuracy of cryocooler system is within 10mK, and it obtains certain robustness.
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星载高精度制冷机控制系统研究
针对遥感相机焦平面精确温度要求(mK级),设计了一种基于脉冲管制冷机的高精度温度控制系统。为了提高温度的控制精度,首先介绍了恒流源电路的设计,并结合温度控制要求给出了恒流源的精度要求。其次,设计了两级放大电路和滤波器,并给出了参数的选择方法。最后,介绍了增量式PID控制算法,给出了真空环境下温度控制的数值实验结果:(1)给出了不同温度控制点下制冷机系统的闭环精度,温度控制精度均在10mK以内;(2)当制冷机系统热板温度在5℃以内变化时,制冷机系统再次达到稳定状态,稳态误差仍在10mK以内。实验结果表明,制冷机系统的闭环控制精度在10mK以内,并具有一定的鲁棒性。
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