| 反雷达导弹惯性末制导基准轴误差的修正 |
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| 引用本文： | 刘育华,崔乃刚,刘暾.反雷达导弹惯性末制导基准轴误差的修正[J].航天控制,1991(1). |
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| 作者姓名： | 刘育华 崔乃刚 刘暾 |
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| 作者单位： | 哈尔滨工业大学，哈尔滨工业大学，哈尔滨工业大学 |
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| 摘 要： | 本文采用广义卡尔曼滤波方法解决空地反雷达导弹抗雷达关机方案中出现的惯性末制导基准轴指向误差的修正这一问题。最后举出了导弹运动模型的实例。
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| 关 键 词： | 反雷达导弹 卡尔曼滤波 制导误差 校正 |
THE CORRECTION FOR THE BASIC AXIS ERROR OF THE INERTIAL TERMINAL GUIDANCE ON THE ANTIRADAR MISSILE |
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| Liu Yuhua Chui Naigang Liu Dun Harbin Lnstitute of Technology.THE CORRECTION FOR THE BASIC AXIS ERROR OF THE INERTIAL TERMINAL GUIDANCE ON THE ANTIRADAR MISSILE[J].Aerospace Control,1991(1). |
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| Authors: | Liu Yuhua Chui Naigang Liu Dun Harbin Lnstitute of Technology |
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| Institution: | Liu Yuhua Chui Naigang Liu Dun Harbin Lnstitute of Technology |
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| Abstract: | In this paper, a generalized kalman filtering method is used on an air to ground antiradar missile to slove the correction problem for the basic axis direction error of inertial terminal gnidance. Finally, a practical example about the missile motion model is given. |
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| Keywords: | Antiradar missile Kalmanfilter Guidance error Correction |
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