首页 | 本学科首页   官方微博 | 高级检索  
     检索      

卫星姿态控制系统容错控制综述
引用本文:姜斌,张柯,杨浩,程月华,马亚杰,成旺磊.卫星姿态控制系统容错控制综述[J].航空学报,2021,42(11):524662-524662.
作者姓名:姜斌  张柯  杨浩  程月华  马亚杰  成旺磊
作者单位:南京航空航天大学 自动化学院,南京 211106
基金项目:国家自然科学基金(62020106003,62073165,61773201);江苏省杰出青年基金(BK20200015);111引智基地项目(B20007);江苏高校"青蓝工程
摘    要:主要针对卫星姿态系统容错控制研究领域已有的成果进行了回顾。总结了国内外卫星容错控制的现有成果,主要从卫星姿态控制系统的可重构性、单体卫星容错控制和卫星编队容错控制3个部分对相关的研究成果进行了归纳分析。其中,卫星姿态系统的可重构性从重构目标和系统功能要求两方面进行分析;对单体卫星容错控制现状的介绍主要从自适应技术、滑模理论、预设性能、干扰观测器、故障估计观测器几个方面展开;卫星编队容错控制方法从独立容错、协同容错、拓扑重构和组成重构的角度进行阐述。最后进行总结,并展望了卫星姿态控制系统容错控制领域未来可能出现的新问题和研究思路。

关 键 词:卫星姿态控制系统  可重构性  容错控制  卫星编队  暂态与稳态性能
收稿时间:2020-08-22
修稿时间:2020-09-23

Fault-tolerant control of satellite attitude control systems: Review
JIANG Bin,ZHANG Ke,YANG Hao,CHENG Yuehua,MA Yajie,CHENG Wanglei.Fault-tolerant control of satellite attitude control systems: Review[J].Acta Aeronautica et Astronautica Sinica,2021,42(11):524662-524662.
Authors:JIANG Bin  ZHANG Ke  YANG Hao  CHENG Yuehua  MA Yajie  CHENG Wanglei
Institution:College of Automation Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 211106, China
Abstract:The achievements in the research field of fault-tolerant control of satellite attitude systems are reviewed. The results of satellite attitude fault-tolerant control at home and abroad are summarized and analyzed from three parts:the reconfigurability of satellite attitude systems, single satellite fault-tolerant control, and satellite formation fault-tolerant control. The reconfigurability of the satellite attitude system is analyzed from two aspects:reconstruction goals and system functional requirements. The introduction of the current status of single satellite fault-tolerant control mainly includes the adaptive technology, sliding mode theory, prescribed performance, disturbance observer and fault estimation observer. The satellite formation fault-tolerant control methods are explained from the perspectives of independent fault tolerance, cooperative fault tolerance, topology reconstruction, and composition reconstruction. Finally, a summary of this article is provided, and new problems and research ideas in fault-tolerant control of satellite attitude control systems are prospected.
Keywords:satellite attitude control systems  reconfigurability  fault-tolerant control  satellite formation  transient and steady-state performances  
本文献已被 万方数据 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号