A Review on Recent Development of Spacecraft Attitude Fault Tolerant Control System
A Review on Recent Development of Spacecraft Attitude Fault Tolerant Control System
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DOI：
10.1109/tie.2016.2530789
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发表时间：
2016-02
影响因子：
7.7
通讯作者：
Shen Yin;B. Xiao;S. Ding;Donghua Zhou
中科院分区：
文献类型：
--
作者：
Shen Yin;B. Xiao;S. Ding;Donghua Zhou
受几起事故的影响，航天器故障/失效的姿态控制问题引起了航天工程界和学术界的广泛关注。本文研究航天器姿态控制系统的容错控制和故障检测与诊断的工业实践和理论方法。综述了航天器姿态FTC系统设计的最新进展。介绍了FTC系统的基本原理。讨论了现有的工程FTC技术和理论方法，包括它们的优点和缺点。此外，密切相关的可靠性相关的问题，最近的态度FTC设计策略的进展进行了审查。简要回顾了航天器姿态控制设计中的一些开放性问题，并进一步总结了组件故障/失效。
Motivated by several accidents, attitude control of a spacecraft subject to faults/failures has gained considerable attention in a wider range of aerospace engineering and academic communities. This paper is concerned with industrial practices and theoretical approaches for fault tolerant control (FTC) and fault detection and diagnosis (FDD) in spacecraft attitude control system. An overview on recent development of spacecraft attitude FTC system design is presented. The basis of a FTC system is introduced. The existing engineering FTC techniques and theoretical methodologies, including their advantages and disadvantages, are discussed. Moreover, closely associated with the reliability-relevant issues, recent progress in attitude FTC design strategies is reviewed. A brief review of some open problems in the general area of spacecraft attitude control design subject to components faults/failures is further concluded.