| 一种巡航导弹组合高度方案设计 |
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| 引用本文： | 吴天,张胜修,颜诗源.一种巡航导弹组合高度方案设计[J].控制工程,2007(Z2). |
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| 作者姓名： | 吴天 张胜修 颜诗源 |
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| 作者单位： | 第二炮兵工程学院303教研室 陕西西安710025 |
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| 摘 要： | 针对惯性高度通道、气压高度表和雷达高度表在巡航导弹高度测量中的优缺点,根据组合高度的思想,采用卡尔曼滤波的信息融合技术,将三者有机地结合起来,取长补短,实现高度测量。仿真结果表明,气压/惯性/雷达的组合方案可以有效提高高度系统测量精度,增强巡航导弹的稳定性能。
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| 关 键 词： | 巡航导弹 组合高度 卡尔曼滤波 |
Design of Combined Altitude Project for Cruise Missile |
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| WU Tian,ZHANG Sheng-xiu,YAN Shi-yuan.Design of Combined Altitude Project for Cruise Missile[J].Control Engineering of China,2007(Z2). |
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| Authors: | WU Tian ZHANG Sheng-xiu YAN Shi-yuan |
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| Abstract: | To the advantages and disadvantages of inertial vertical channel,baro-altimeter and radar altimeter in height measurement system for cruise missile,based on the idea of combined altitude,Kalman filter is adopted to integrate these three altimeters,which can overcome the shortcomings while exerting the advantages of each.The simulation results show that the combined altitude scheme can effectively improve the precision of height measurement system,and enhance stability of cruise missile. |
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| Keywords: | cruise missile combined altitude Kalman filter |
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