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低测量精度限制下的航天器高精度控温方法

乐述文 张晓峰 冯建朝 吴文锋

北京航空航天大学学报2026,Vol.52Issue(8):2780-2787,8.
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北京航空航天大学学报2026,Vol.52Issue(8):2780-2787,8.DOI:10.13700/j.bh.1001-5965.2025.0583

低测量精度限制下的航天器高精度控温方法

Precise temperature control method for spacecraft under low measurement accuracy constraints

乐述文 1张晓峰 1冯建朝 2吴文锋2

作者信息

  • 1. 中国科学院微小卫星创新研究院,上海 201304
  • 2. 中国科学院微小卫星创新研究院,上海 201304||中国科学院大学 星际航行学院,北京 100049
  • 折叠

摘要

Abstract

To meet the demand for precise temperature control in spacecraft under the constraint of low temperature measurement resolution,this paper proposes a high-precision temperature control method based on Kalman filtering(KF).This method first constructs a thermal model of the controlled object.The Kalman filter algorithm is then utilized to estimate temperature state changes and suppress temperature measurement noise.Finally,closed-loop control based on the filtered data is implemented to achieve high-precision temperature regulation.A modified Kalman filter(mKF)approach that incorporates continuous correction based on moving average filter results is suggested in order to address the problem of parameter adjustment inherent in this method.Through experiments and simulations,the influence of parameter settings on temperature control accuracy was analyzed.The findings demonstrate that the temperature control system using Kalman filtering improves control accuracy and adaptability to larger PI parameter values under the constraint of a temperature measurement resolution lower than 100 mK,achieving a stability better than 10 mK across a wider parameter range.After applying the modified Kalman Filtermethod,the system's temperature control accuracy under large PI control parameters is further improved.Moreover,the system exhibits lower sensitivity to PI control parameters,filtering parameters,and thermal model parameters,resulting in reduced parameter tuning difficulty and enhanced robustness.

关键词

测温分辨力/温度控制/卡尔曼滤波/参数整定/鲁棒性

Key words

temperature resolution/temperature control/Kalman filtering/parameter tuning/robustness

分类

航空航天

引用本文复制引用

乐述文,张晓峰,冯建朝,吴文锋..低测量精度限制下的航天器高精度控温方法[J].北京航空航天大学学报,2026,52(8):2780-2787,8.

基金项目

国家重点研发计划(2022YFC2204300) National Key Research and Development Program of China(2022YFC2204300) (2022YFC2204300)

北京航空航天大学学报

1001-5965

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