| 空空导弹动基座低成本传递对准技术研究 |
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| 引用本文： | 周叶,杨莉,汪叔华.空空导弹动基座低成本传递对准技术研究[J].南京航空航天大学学报,1999,31(1):116-120. |
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| 作者姓名： | 周叶 杨莉 汪叔华 |
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| 作者单位： | 南京航空航天大学自动控制系,南京,210016 |
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| 摘 要： | 针对空空导弹的特点，采用低成本惯性器件实现其动基座对准，文中重点研究了主惯导为平台式的惯导系统，子惯导为捷联式的惯导系统的传递对准原理和精度计算方法；建立了传递对准数学模型，进行了仿真研究；给出了具有实际参考价值的对准方案
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| 关 键 词： | 惯性导航系统 卡尔曼滤波 传递对准 |
| 修稿时间： | 1998-05-25 |
Study on Low-Cost Transfer Alignment for Missile on Moving Base |
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| Zhou Ye,Yang Li,Wang Shuhua.Study on Low-Cost Transfer Alignment for Missile on Moving Base[J].Journal of Nanjing University of Aeronautics & Astronautics,1999,31(1):116-120. |
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| Authors: | Zhou Ye Yang Li Wang Shuhua |
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| Abstract: | Due to the characteristics of the missile, the low cost inertial apparatus is applied. The master inertial navigation system (INS) is platform INS and the slave INS a strapdown INS. The transfer alignment theory and the calculation method of precision are emphasized. The mathematics model of the transfer alignment and the alignment scheme is established. The simulation provides the alignment scheme having the actual reference va lue. |
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| Keywords: | inertial navigation system Kalman filtering transfer alignment |
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