循环热管温度控制的扩展非线性动力学建模与状态估计

Thomas Gellrich, Jonas Moeller, S. Schwab, S. Hohmann
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引用次数: 0

摘要

对于航天系统的热控制,回路热管(LHPs)常被用作被动的两相热传输系统。它们的高传热系数是通过工作流体的蒸发和冷凝达到的,其在回路中的质量流动是由多孔芯中的毛细力建立的。然而,LHP的工作温度取决于热源的散热量和散热器的温度。因此,在LHP的补偿室上的加热器可以在不同的操作条件下控制温度。为了在实际lhp上实现所设计的状态相关非线性控制器,本文设计了一种基于平方根无气味卡尔曼滤波器(SR-UKF)的非线性动态状态估计。该过滤器为控制器提供所需的LHP状态。在此基础上,通过对LHP内部过热蒸汽的建模,将LHP的非线性状态空间模型扩展到4个温度测量值。数值仿真结果表明,扩展LHP状态空间模型提高了控制性能,对不同工况具有较高的鲁棒性。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Extended Nonlinear Dynamical Modeling and State Estimation for the Temperature Control of Loop Heat Pipes
For the thermal control of aerospace systems, loop heat pipes (LHPs) are often utilized as passive, two-phase heat transport systems. Their high heat transfer coefficient is reached through evaporation and condensation of a working fluid, whose mass flow in the loop is established by capillary forces in a porous wick. However, the LHP operating temperature depends on the dissipated heat of the heat sources and the temperature of the heat sink. Thus, a heater on the compensation chamber of the LHP enables the temperature control under varying operating conditions. To realize the designed state-dependent nonlinear controller on actual LHPs, a nonlinear dynamical state estimation based on the square-root unscented Kalman filter (SR-UKF) is designed in this paper. This filter provides the controller with the required LHP states. Furthermore, the underlying nonlinear LHP state-space model with two temperature measurement is extended to four temperature measurements by modeling the overheated vapor in the LHP. It is shown in a numerical LHP simulation that the extended LHP state-space model improves the control performance achieving a higher robustness against the varying operating conditions.
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