电推进在航天器姿态控制中的研究综述  

A Review of Research on Electric Propulsion in Spacecraft Attitude Control

作　　者：贾英宏[1] 孟文沁 JIA Ying-hong;MENG Wen-qin(School of Astronautics,Beihang University,Beijing 100191,China)

机构地区：[1]北京航空航天大学宇航学院,北京100191

出　　处：《推进技术》2023年第7期98-113,共16页Journal of Propulsion Technology

摘　　要：本文首先对电推进技术进行了简要的介绍,根据目前已有的电推进姿态控制应用,分析了适用于航天器姿态控制的不同类型的电推力器特性,之后分别对电推力器在姿态控制中的在轨应用现状和研究现状进行了综述和分析。在研究现状综述中,针对航天器姿态控制、姿轨联合控制和角动量卸载三个任务类型,分析总结了电推力器在布局、控制策略和算法等方面的研究成果和结论。最后,针对未来电推进技术在航天器姿态控制应用所面临的挑战,提出了相应的发展建议。This paper presents a review on electric propulsion technology in spacecraft attitude control.Firstly,the general electric propulsion technology is introduced,and the characteristics of different types of electric thrusters suitable for attitude control are analyzed.Then,the on-orbit application status and the re⁃search status of electric thrusters in spacecraft attitude control are reviewed respectively.In the review of re⁃search status,the research results and conclusions of electric thrusters in thruster layout,control strategy and control algorithm are analyzed and summarized oriented to three tasks which including spacecraft attitude con⁃trol,joint attitude and orbit control,and angular momentum unloading.Finally,corresponding development suggestions are proposed for the challenges of electric propulsion technology in the future application of space⁃craft attitude control.

关 键 词：电推进 姿态控制 角动量卸载 姿轨联合控制 电推力器布局 综述 

分 类 号：V439.4[航空宇航科学与技术—航空宇航推进理论与工程] V11