| 高超声速巡航飞行器中制导研究 |
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| 引用本文： | 李惠峰,陈金栋,李娜英. 高超声速巡航飞行器中制导研究[J]. 现代防御技术, 2006, 34(6): 61-65 |
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| 作者姓名： | 李惠峰 陈金栋 李娜英 |
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| 作者单位： | 北京航空航天大学,宇航学院,北京,100083 |
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| 摘 要： | 通过分析目前应用较为普遍的几种组合导航方式,针对高超声速巡航飞行器,提出了采用捷联惯性导航系统(SINS)/GPS/天文导航系统(CNS)组合导航作为其中段制导方案,并利用四元数法进行捷联惯性导航计算,运用联邦滤波方法对组合导航进行了仿真,仿真结果表明该方案行之有效。
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| 关 键 词： | 高超声速巡航飞行器 组合式导航 中制导 联邦滤波 |
| 文章编号： | 1009-086X(2006)-06-0061-05 |
| 修稿时间： | 2006-01-03 |
Research on midcourse navigation of hypersonic cruise air vehicles |
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| LI Hui-feng,CHEN Jin-dong,LI Na-ying. Research on midcourse navigation of hypersonic cruise air vehicles[J]. Modern Defence Technology, 2006, 34(6): 61-65 |
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| Authors: | LI Hui-feng CHEN Jin-dong LI Na-ying |
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| Abstract: | Through analyzing several common integrated navigation systems,the navigation method for hypersonic cruise air vehicles were put forward by adopting strapdown inertial navigation system(SINS)/GPS/celestial navigation system(CNS) .With quaternion in strapdown inertial navigation,the combined navigation system by means of federated Kalman filtering method was simulated.The simulation results showed that the system is feasible and effective. |
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| Keywords: | hypersonic cruise air vehicle combined navigation midcourse navigation federated filtering |
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