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组合导航制导系统的容错技术及特点
引用本文:周露,闻新.组合导航制导系统的容错技术及特点[J].上海航天,1999,16(2):58-61.
作者姓名:周露  闻新
作者单位:北京师范大学数学系(周露),北京空间飞行器总体设计部(闻新),航天总公司二院208所(周秀芬)
摘    要:论述了组合导航制导系统的容错设计方案,其中包括INS/GPS(惯性导航/全球定位系统)组合系统容错技术、SINS/GPS/多普勒组合系统的容错技术及INS/GPS/CNS组合系统的容错技术;然后分析了组合导航制导系统的抗故障问题,给出了组合导航、制导系统的故障分类和系统出故障后的运用情况;最后,对其发展进行了展望,并提出了今后有待进一步研究的问题。

关 键 词:组合导航,制导  容错技术  故障诊断  可靠性

THE FAULT TOLERANT TECHNOLOGY AND PROPERTY ON INTEGRATED NAVIGATION GUIDANCE
ZHOU Lu ,WEN Xin ,ZHOU Xiu fen.THE FAULT TOLERANT TECHNOLOGY AND PROPERTY ON INTEGRATED NAVIGATION GUIDANCE[J].Aerospace Shanghai,1999,16(2):58-61.
Authors:ZHOU Lu  WEN Xin  ZHOU Xiu fen
Institution:ZHOU Lu 1,WEN Xin 2,ZHOU Xiu fen 3
Abstract:The fault tolerant schemes on integrated navigation guidance systems are discussed. Discussed contents included the fault tolerant technology of INS/GPS integrated system, SINS/GPS/Doppler integrated system and INS/GPS/CNS integrated system. Then, the fault resistant properties on integrated navigation guidance are analyzed. Last, the future development of this technique is forecasted, and the problems to be studied are pointed out.
Keywords:Integrated navigation  Guidace  Fault  tolerant technique  Fault diagnosis  Reliability
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