摆动式红外地球敏感器故障建模与仿真

系统仿真学报 ›› 2016, Vol. 28 ›› Issue (1): 8-18.

摆动式红外地球敏感器故障建模与仿真

常建松^1,2, 刘新彦¹

1.北京控制工程研究所,北京 100190;
2.空间智能控制技术重点实验室,北京 100190

收稿日期:2014-08-26 修回日期:2014-10-21 发布日期:2020-07-02
作者简介:常建松(1982-),男,黑龙江,高工,研究方向为卫星控制系统方案设计与仿真;刘新彦(1970-),男,山西,研究员,研究方向为航天器控制系统总体设计。
基金资助:
国家自然科学基金资助项目(61203093); 国家自然科学基金资助项目(61203093)

Fault Modeling and Simulation of Swing Infrared Earth Sensor

Chang Jiansong^1,2, Liu Xinyan¹

1. Beijing Institute of Control Engineering, Beijing 100190, China;
2. Science and Technology on Space Intelligent Control Laboratory, Beijing 100190, China

Received:2014-08-26 Revised:2014-10-21 Published:2020-07-02

摘要/Abstract

摘要： 为满足精细化建模和故障仿真验证需求,根据摆动式红外地球敏感器的工作原理,对其进行功能模块划分,分析各模块主要故障模式,建立基于物理机理的故障数学模型,编写仿真程序进行正常和故障仿真验证。结果表明所建立的地球敏感器精细化故障模型,能够正确计算姿态角,反映内部各模块间信息传递关系,还能有效地模拟各种故障模式,可以应用于卫星控制系统仿真测试和故障诊断等方面。

关键词: 红外地球敏感器, 模块划分, 故障模式分析, 故障建模, 仿真验证

Abstract: In order to meet the requirements of refined modeling and fault simulation, function modules of swing infrared earth sensor (IRES) was identified according to its working principle, main fault modes of each module was analyzed, mathematical fault model based on physical mechanism was designed, and a program for normal and fault simulation was written. The refined fault model can calculate attitude angles exactly, reflect signal relationship between inside modules, and simulate various fault modes effectively. The model can be used in simulating, testing and fault diagnosis and so on.

Key words: infrared earth sensor, module identification, fault mode analysis, fault modeling, simulation

中图分类号:

常建松, 刘新彦. 摆动式红外地球敏感器故障建模与仿真[J]. 系统仿真学报, 2016, 28(1): 8-18.

Chang Jiansong, Liu Xinyan. Fault Modeling and Simulation of Swing Infrared Earth Sensor[J]. Journal of System Simulation, 2016, 28(1): 8-18.

参考文献

[1] 屠善澄. 卫星姿态动力学与控制 3册 [M]. 北京: 宇航出版社, 2003: 73-77.
[2] 唐尧. 考虑高度参数的摆动式红外地球敏感器模型研究[J]. 空间控制技术与应用, 2012, 38(3): 27-32.
(TANG Yao.Research on Swing Scanning Infrared Earth Sensor with Orbit Altitude Concerned[J]. Aerospace Control and Application (S1674-1579), 2012, 38(3): 27-32.)
[3] 雷仲谋, 李建平, 陈国宇. 摆动式扫描红外地球敏感器在轨探头级备份工作研究[J]. 空间控制技术与应用, 2013, 39(6): 40-44.
(LEI Zhongmou, LI Jianping, CHEN Guoyu.On Bolometer Detector Redundancy of Swing Infraed Earth Sensor[J]. Aerospace Control and Application (S1674-1579), 2013, 39(6): 40-44.)
[4] 王行仁, 文传源, 李伯虎, 等. 我国系统建模与仿真技术的发展[J]. 系统仿真学报, 2009, 21(21): 6683-6688.
(WANG Xingren, WEN Chuanyuan, LI Bohu, et al.The Development of System Modeling and Simulation Technologies in China[J]. Journal of System Simulation (S1004-731X), 2009, 21(21): 6683-6688.)
[5] 欧阳高翔, 倪茂林, 孙承启等. 航天器的故障建模与应用[J]. 航天控制, 2011, 29(5): 22-29.
(Ouyang Gaoxiang, Ni Maolin, Sun Chengqi, et al.The Fault Modeling and Application to Aerospace Engineering[J]. Aerospace Control (S1006-3242), 2011, 29(5): 22-29.)
[6] 刘新彦, 常建松. 某型动量轮精细化故障建模研究[C]// 全国第十六届空间及运动体控制技术学术会议论文集, 北京: 北京控制工程研究所, 2014: 535-541.
[7] 吕超, 刘爽, 王世明. 基于机构原理的设备模块划分与耦合决策方法[J]. 系统仿真学报, 2014, 26(4): 739-743.
(Lv Chao, Liu Shuang, Wang Shiming.Method of Module Division and Coupling Decision Based on Mechanism Theory[J]. Journal of System Simulation (S1004-731X), 2014, 26(4): 739-743.)
[8] Liu Rui, Zhou Jun, Li Peng.A Method for Components Fault Model Building[C]// 2012 4th International Conference on Mechanical and Electronics Engineering. Switzerland: Trans Tech Publications, 2012: 156-159
[9] 张孝功, 任章. 一种卫星故障诊断的定性/定量混合建模新方法[J]. 空间控制技术与应用, 2009, 35(5): 38-42.
(Zhang Xiaogong, Ren Zhang.A New Modeling Method of Satellite Fault Diagnosis Based on the Qualitative/ Quantitative Hybird Model. Aerospace Control and Application (S1674-1579), 2009, 35(5): 38-42.)
[10] 常建松, 郭建新, 李艳华, 等. IGSO卫星地球敏感器受南极红外辐射波动影响分析[C]// 中国宇航学会飞行器总体专业委员会第12届学术研讨会论文集, 北京: 中国空间技术研究院, 2012: 206-209.