卫星姿态控制系统故障预测方法综述  

Review of Fault Prediction Methods for Satellite Attitude Control System

作　　者：曲直 张高飞 孟子阳[1] 许瑞钦 QU Zhi;ZHANG Gaofei;MENG Ziyang;XU Ruiqin(Department of Precision Instrument,Tsinghua University,Beijing 100084,China;School of Instrumentation Science and Optoelectronic Engineering,Beijing Information Science and Technology University,Beijing 100192,China)

机构地区：[1]清华大学精密仪器系,北京100084 [2]北京信息科技大学仪器科学与光电工程学院,北京100192

出　　处：《宇航学报》2023年第6期829-840,共12页Journal of Astronautics

基　　金：空间智能控制技术重点实验室基金(2021JCJQLB01016)。

摘　　要：结合目前卫星姿态控制系统(ACS)故障预测技术的迫切需求,回顾了故障预测技术研究进展,归纳梳理了知识驱动方法和数据驱动方法的特点,总结并指出了卫星姿态控制系统故障预测技术面临的技术难点。在此基础上,重点阐述了知识和数据联合驱动方法在当前和未来的关键问题与解决途径,从知识和数据并行模式、引导模式、反馈模式三个分支给出了相应关键技术后续发展的方向与思路。Combined with the urgent needs of satellite attitude control system(ACS)fault prediction technology,the research progress of fault prediction technology is reviewed,the characteristics of knowledge-driven and data-driven methods are summarized and the technical dfficulties faced by satellite ACS fault prediction technology are pointed out.On this basis,the key problems and solutions of the joint knowledge and data-driven methods in the present and future are expounded,and the subsequent development directions and ideas of the corresponding key technologies are given from the three aspects of knowledge and data parallel mode,guidance mode and feedback mode.

关 键 词：卫星控制 姿态控制系统 故障预测技术 知识与数据联合驱动方法 并行、引导和反馈模式 

分 类 号：V19[航空宇航科学与技术—人机与环境工程]