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航天器控制系统可重构性的内涵与研究综述

王大轶 屠园园 刘成瑞 何英姿 李文博

王大轶, 屠园园, 刘成瑞, 何英姿, 李文博. 航天器控制系统可重构性的内涵与研究综述. 自动化学报, 2017, 43(10): 1687-1702. doi: 10.16383/j.aas.2017.c160700
引用本文: 王大轶, 屠园园, 刘成瑞, 何英姿, 李文博. 航天器控制系统可重构性的内涵与研究综述. 自动化学报, 2017, 43(10): 1687-1702. doi: 10.16383/j.aas.2017.c160700
WANG Da-Yi, TU Yuan-Yuan, LIU Cheng-Rui, HE Ying-Zi, LI Wen-Bo. Connotation and Research of Reconfigurability for Spacecraft Control Systems:A Review. ACTA AUTOMATICA SINICA, 2017, 43(10): 1687-1702. doi: 10.16383/j.aas.2017.c160700
Citation: WANG Da-Yi, TU Yuan-Yuan, LIU Cheng-Rui, HE Ying-Zi, LI Wen-Bo. Connotation and Research of Reconfigurability for Spacecraft Control Systems:A Review. ACTA AUTOMATICA SINICA, 2017, 43(10): 1687-1702. doi: 10.16383/j.aas.2017.c160700

航天器控制系统可重构性的内涵与研究综述

doi: 10.16383/j.aas.2017.c160700
基金项目: 

国家自然科学基金 61640304

国家自然科学基金 61573060

国家自然科学基金 61690215

国家杰出青年科学基金 61525301

国家自然科学基金 61203093

详细信息
    作者简介:

    屠园园 北京控制工程研究所博士研究生.2014年于哈尔滨工业大学获学士学位.主要研究方向为卫星控制系统的可重构性评价与设计.E-mail:tyyfti@163.com

    刘成瑞 北京控制工程研究所高级工程师.2006年在北京航空航天大学获博士学位.主要研究方向为卫星控制系统的故障诊断与容错控制.E-mail:liuchengrui@gmail.com

    何英姿 北京控制工程研究所研究员.主要研究方向为航天器制导与控制.E-mail:heyz1970@163.com

    李文博 北京控制工程研究所高级工程师.2012年在哈尔滨工业大学获博士学位.主要研究方向为故障诊断与容错控制, 卫星控制系统的可诊断性评价与设计.E-mail:liwenbo bice@163.com

    通讯作者:

    王大轶 北京空间飞行器总体设计部研究员.主要研究方向为航天器的自主制导、导航与控制, 故障诊断与容错控制.本文通信作者, E-mail:dayiwang@163.com

Connotation and Research of Reconfigurability for Spacecraft Control Systems:A Review

Funds: 

National Natural Science Foundation of China 61640304

National Natural Science Foundation of China 61573060

National Natural Science Foundation of China 61690215

National Science Fund for Distinguished Young Scholars 61525301

National Natural Science Foundation of China 61203093

More Information
    Author Bio:

    Ph. D. candidate at Beijing Institute of Control Engineering. She received her bachelor degree from Harbin Institute of Technology in 2014. Her research interest covers reconflgurability evaluation and design for satellite control systems

    Senior engineer at Beijing Institute of Control Engineering. He received his Ph. D. degree from Beijing University of Aeronautics and Astronautics in 2006. His research interest covers fault diagnosis and tolerant control for spacecrafts

    Professor at Beijing Institute of Control Engineering. Her research interest covers guidance and control for spacecrafts

    Senior engineer at Beijing Institute of Control Engineering. He received his Ph. D. degree from Harbin Institute of Technology in 2012. His research interest covers fault diagnosis and tolerant control, fault diagnosability evaluation and design for satellite control systems

    Corresponding author: WANG Da-Yi  Professor at Beijing Institute of Spacecraft System Engineering. His research interest covers autonomous guidance, navigation and control, fault diagnosis, and tolerant control for spacecrafts. Corresponding author of this paper, E-mail:dayiwang@163.com
  • 摘要: 可重构性设计是提高航天器在轨运行质量的有效途径,可以从系统层面克服航天器控制系统固有可靠性不足、星上资源受限以及在轨故障不可维修等缺陷,目前已引起控制理论和航天器控制工程等领域的高度重视与广泛关注.本文首先结合航天器控制系统的固有特点,具体介绍可重构性的研究意义与概念内涵.然后从评价与设计两方面,详细梳理航天器控制系统可重构性的研究内容与研究现状.最后对目前可重构性研究领域中存在的一些问题以及未来可能的发展方向进行深入探讨.
    1)  本文责任编委 孙富春
  • 图  1  重构控制过程的时间响应

    Fig.  1  Time response during control reconfiguration

    图  2  航天器控制系统可重构性的研究内容

    Fig.  2  Research contents of reconfigurability of spacecraft control system

    表  1  可靠性与可重构性的对比分析

    Table  1  The comparative analysis of reliability and reconfigurability

    可靠性可重构性
    研究范畴系统运行质量特性
    研究对象统计特性功能特性
    研究目的预防故障处理故障
    优化手段提高冗余量优化冗余分配
    时间维度 $\surd$
    空间维度2(逻辑关系)3(空间构型)
    限制因素生产因素
    (成本/重量/工艺)
    性能因素
    (资源/时间/输出)
    下载: 导出CSV

    表  2  控制可重构性评价方法对比

    Table  2  Comparison of different control reconfigurability evaluation methods

    思路优点不足
    基于系统
    固有特性
    基于一般控制理论, 通用
    性强, 物理意义明确
    未考虑实际限制约束
    基于系统
    性能约束
    考虑各项性能约束, 更具
    工程实际意义
    各项约束综合方
    法尚无统一标准
    基于系统
    功能要求
    可用于大型复杂系统运算量大、模型
    复杂, 依靠经验
    下载: 导出CSV
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  • 收稿日期:  2016-10-09
  • 录用日期:  2017-05-06
  • 刊出日期:  2017-10-20

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