| 飞航导弹INS／GPS组合制导仿真分析 |
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| 引用本文： | 杨勇,赵晶,张文明.飞航导弹INS／GPS组合制导仿真分析[J].战术导弹技术,2009(4):56-58,72. |
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| 作者姓名： | 杨勇 赵晶 张文明 |
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| 作者单位： | 国防科技大学,长沙410073 |
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| 摘 要： | 介绍了INS／GPS组合导航在飞航导弹制导中的应用，结合假定弹道，对飞航导弹INS／GPS组合导航系统信息处理过程进行了建模与仿真，分析了陀螺漂移、GPS定位精度对INS／GPS组合导航系统制导精度的影响。
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| 关 键 词： | INS GPS 飞航导弹 |
Simulation of INS/GPS Integrated Navigation in Aerodynamic Missile |
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| Yang Yong,Zhao Jing,Zhang Wenming.Simulation of INS/GPS Integrated Navigation in Aerodynamic Missile[J].Tactical Missile Technology,2009(4):56-58,72. |
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| Authors: | Yang Yong Zhao Jing Zhang Wenming |
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| Affiliation: | ( National University of Defence Technology, Changsha 410073, China) |
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| Abstract: | INS/GPS integrated navigation used in aerodynamic missile is introduced. The signal processing of INS/GPS integrated navigation system in aerodynamic missile is modeled and simulated. The influ ences of gyro drift and GPS positioning accuracy on the positioning accuracy of INS/GPS integrated navigation system are analyzed. |
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| Keywords: | INS GPS aerodynamic missile |
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