Volume 31 Issue 2
Feb.  2006
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KANG Guohua, LIU Jianye, XIONG Zhi, ZHU Yanhua. GNSS/ SST/SINS Integrated Navigation System for Ballistic Missile[J]. Geomatics and Information Science of Wuhan University, 2006, 31(2): 176-179.
Citation: KANG Guohua, LIU Jianye, XIONG Zhi, ZHU Yanhua. GNSS/ SST/SINS Integrated Navigation System for Ballistic Missile[J]. Geomatics and Information Science of Wuhan University, 2006, 31(2): 176-179.
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GNSS/ SST/SINS Integrated Navigation System for Ballistic Missile

  • 1 Navigation Research Center,Nanjing University of Aeronautics and Astronautics,29 Yudao Street,Nanjing 210016,China

Funds: 国家自然科学基金资助项目(60472125)
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  • Received Date: November 26, 2005
  • Revised Date: November 26, 2005
  • Published Date: February 04, 2006
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  • This paper presents a new integrated project,which uses strapdown sensors and fuses the information of the attitude of strapdown star tracker(SST),the position and velocity of the high speed GNSS and the corresponding information of SINS to filter.Meanwhile the design of the simulated real-time GNSS/ST/SINS platform has been realized.The result shows that the system is robust and reliable.
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