| REALIZATION OF GPS／SST／SINS INTEGRATED NAVIGATION FILTER ALGORITHM FOR BALLISTIC MISSILE |
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| 引用本文： | KANGGuo-hua LIUJian-ye ZHUYan-hua XIONGZhi. REALIZATION OF GPS／SST／SINS INTEGRATED NAVIGATION FILTER ALGORITHM FOR BALLISTIC MISSILE[J]. 勤云标准版测试, 2005, 0(2): 115-118 |
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| 作者姓名： | KANGGuo-hua LIUJian-ye ZHUYan-hua XIONGZhi |
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| 作者单位： | CollegeofAutomationEngineering,NUAA,29YudaoStreet,Nanjing,210016,P.R.China |
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| 摘 要： | Considering the domestic single navigation system of the ballistic missile, a new filter method is presented. The method integrates the information of the strapdown star tracker (SST) attitude, the position and the velocity of a high speed GPS with a strapdown inertial navigation system (SINS) information into one filter, thus improving the precision of the attitude, the velocity, and the position. Finally, the GPS/SST/SINS simulation platfornt is designed. Simulation results demonstrate that the filter is robust and reliable, and the precision rises to the comparative level abroad.
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| 关 键 词： | GPS 弹道导弹 组合制导 导航滤波算法 |
REALIZATION OF GPS/SST/SINS INTEGRATED NAVIGATION FILTER ALGORITHM FOR BALLISTIC MISSILE |
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