| 方位对准误差对制导精度影响的研究 |
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| 引用本文： | 朱绍箕.方位对准误差对制导精度影响的研究[J].航天控制,1990(1). |
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| 作者姓名： | 朱绍箕 |
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| 作者单位： | 北京自动化控制设备研究所 |
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| 摘 要： | 本文分析了在不同发射条件下,惯性导航系统方位对准误差对制导精度的影响。研究结果表明,对于空射型导弹,惯性导航系统方位对准误差对制导精度的影响与地面发射时有很大的不同,因而可以降低对方位对准精度的要求。
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| 关 键 词： | 瞄准 惯性制导系统 制导误差 地面发射导弹 空中发射导弹 |
A STUDY OF THE EFFECT OF AZIMUTH ALIGNMENT ERROR ON GUIDANCE ACCURACY |
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| Zhu Shaoji Beijing Research Institute of Automation and Control Equipment.A STUDY OF THE EFFECT OF AZIMUTH ALIGNMENT ERROR ON GUIDANCE ACCURACY[J].Aerospace Control,1990(1). |
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| Authors: | Zhu Shaoji Beijing Research Institute of Automation and Control Equipment |
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| Institution: | Zhu Shaoji Beijing Research Institute of Automation and Control Equipment |
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| Abstract: | This paper analyzes the effect of azimuth alignment error of inertial navigation system on the guidance accuracy under different lounching conditions. The research results show that the effect for the air-launched missile is quite different from that for the ground-launched missile. The requirement of the azimurth alignment accuracy of the air-launched missile can be reduced. |
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| Keywords: | Aiming Inertial guidance system Guidance error Ground-lounched missile Air-launched missile Accuracy |
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