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捷联惯导系统(SINS)敏感器斜向配置技术 被引量:2

Redundant Inertial Instruments Configuration for SINS
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摘要 以四个敏感器的冗余系统为例,对采用冗余敏感器的惯导系统的可靠性进行了分析,对四个敏感器构成的捷联惯导系统的可靠性进行了仿真实验,验证了冗余敏感器可以提高系统可靠性结论的正确性。文中给出非正交敏感器测量值向惯导系统正交坐标系转化的方法和转换矩阵。最后对冗余敏感器的配置方式进行了分析。通过仿真实验,得到敏感器最佳配置的条件。 The author analyzes the reliability of SINS and simulates SINS based on the SINS with four redundant inertial instruments. It is proved that the redundant inertial instruments can improve the reliability of SINS. The author presents a new method converting the measurements from the non-orthogonal frame to the orthogonal frame. Finally the result of the optimal configuration of redundant inertial instruments is proved.
出处 《中国惯性技术学报》 EI CSCD 2005年第2期10-13,共4页 Journal of Chinese Inertial Technology
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参考文献4

  • 1Wilcox J C. Competitive evaluation of failure detection algorithm for strapdown redundant inertial instruments[R]. TRW-Final Report, April 1973. 被引量:1
  • 2Krogmann U. Optimal integration of inertial sensor functions for flight control and avionics[A]. AIAA-DASC[C]. San Jose, October 1988. 被引量:1
  • 3Krogmarm U. Design considerations for highly reliable hard and sottware fault tolerant inertial reference systems[A]. Proceedings of DGON Symposium on Gyro Technology[C].Stuttgart, Germany, 1990. 被引量:1
  • 4Harrison J V. Evaluating sensor orientations for navigation performance and failure detection[J]. IEEE Transaction, 1977, AES-13(6). 被引量:1

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