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空间泵驱单相流体回路半物理仿真技术研究

刘东晓 宁献文

航天器环境工程2024,Vol.41Issue(4):414-420,7.
航天器环境工程2024,Vol.41Issue(4):414-420,7.DOI:10.12126/see.2023180

空间泵驱单相流体回路半物理仿真技术研究

Research on hardware-in-the-loop simulation technology for space pumped single-phase fluid loop

刘东晓 1宁献文1

作者信息

  • 1. 北京空间飞行器总体设计部 空间热控技术北京市重点实验室,北京 100094
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摘要

Abstract

In view of the high cost and high risks in conducting full-scale physical experimental validation for space pumped single-phase fluid loop,as well as the challendges in the equivalent simulation of space radiation and heat dissipation behavior in atmospheric environment,a hardware-in-the-loop simulation(HILS)test platform architecture based on CAN bus was proposed.By utilizing a space thermal model to replace some physical entities and integrating ground-based method for equivalent validation of single-phase fluid loop radiator in ambient pressure,the rapid and reliable online validation of the dynamic characteristics of the control system for the space pumped single-phase fluid loop was achieved.The results show that the temperature control accuracy of the system can generally reach±0.5℃under three working conditions.There is little difference in the temperature control performance between conventional PID and neuron PID.The impact of short-term transient high heat flux on the temperature of the control point of main circuit does not exceed 1℃.The proposed research may provide a new technical approach for the development and validation of space pumped single-phase fluid loop control systems.

关键词

单相流体回路/辐射器/散热/热模型/半物理仿真

Key words

single-phase fluid loop/radiator/heat dissipation/thermal model/hardware-in-the-loop simulation

分类

航空航天

引用本文复制引用

刘东晓,宁献文..空间泵驱单相流体回路半物理仿真技术研究[J].航天器环境工程,2024,41(4):414-420,7.

基金项目

国家自然科学基金项目(编号:11472040) (编号:11472040)

航天器环境工程

OACSTPCD

1673-1379

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