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DOI:
飞控与探测:2021,(5):54-61
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运载火箭十表捷联惯组配置的故障诊断与决策
李桂芳1,王 威2,王 鹏2
(1.上海交通大学 电子信息与电气工程学院 上海航天控制技术研究所;2.上海航天控制技术研究所)
Fault Diagnosis and Decision for Launch Vehicle SIMU with 10-Meters Redundancy
LI Guifang1,2, WANG Wei2, WANG Peng2
(1.School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University;2.Shanghai Aerospace Control Technology Institute)
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中文摘要: 容错技术及故障诊断技术是提高导航系统的精度及控制系统的可靠性的有效方法,尤其是捷联导航系统中的故障诊断技术,已经在运载火箭控制系统中得到了广泛的应用。针对运载火箭十表捷联惯组配置,提出了一种故障诊断和决策方法,并在此基础上进行了信息重构方案和故障诊断门限的设计。数学仿真结果表明:该方法能够快速诊断惯性器件表头故障并进行信息重构,实现故障情况下的输出,进而完成飞行任务,对工程应用具有一定的参考价值。
中文关键词: 运载火箭;捷联惯组;故障诊断;十表;可靠性
Abstract:Fault tolerance and diagnosis technology is an effective method to improve the accuracy of the navigation system and the reliability of control system, the fault diagnosis technology in strapdown navigation system has been widely used in the control system of launch vehicle(LV). In this paper, a fault diagnosis and decision method is proposed for the 10-meter-configuration of LV, and on this basis, the scheme of information reconstruction and the threshold of fault diagnosis are designed. The results of mathematical simulation show that the faults of meters can be rapidly diagnosed through this method. It also can output the right information reconstruction of meters in the event of a fault to provide the mission and is worthy for practical engineering applications.
keywords: launch vehicle;SIMU; fault diagnosis; 10-meters-configuration; reliability
文章编号:20210507     中图分类号:TN911.73;TP391.9    文献标志码:A
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作者单位
李桂芳 上海交通大学 电子信息与电气工程学院 上海航天控制技术研究所 
王 威 上海航天控制技术研究所 
王 鹏 上海航天控制技术研究所 
Author NameAffiliation
LI Guifang School of Electronic Information and Electrical Engineering, Shanghai Jiao Tong University
Shanghai Aerospace Control Technology Institute 
WANG Wei Shanghai Aerospace Control Technology Institute 
WANG Peng Shanghai Aerospace Control Technology Institute 
引用文本:
李桂芳,王 威,王 鹏.运载火箭十表捷联惯组配置的故障诊断与决策[J].飞控与探测,2021,(5):54-61.

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