| 空空导弹导引头角预定精度研究 |
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| 引用本文： | 赵洪亮,毛士艺,李少洪.空空导弹导引头角预定精度研究[J].火力与指挥控制,1999,24(1):15-19. |
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| 作者姓名： | 赵洪亮 毛士艺 李少洪 |
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| 作者单位： | 北京航空航天大学,北京,100083 |
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| 基金项目： | 航空工业总公司重点资助课题,航空科学基金 |
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| 摘 要： | 空空导弹导引头角预定是重要的导弹发射控制参数，其有效的计算精度分析，是导弹可靠截获和跟踪目标的重要保证。基于前置追踪攻击原理，给出了空空导弹导引头角预定的计算模型，建立了机载雷达误差对导引头角预定精度影响的误差分析仿真结构，并对仿真计算结果进行了讨论。
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| 关 键 词： | 空空导弹 导弹发射 误差分析 |
The Accuracy Study of Air-to-Air Missile Head Aiming Angles |
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| Zhao Hongliang,Mao Shiyi,Li Shaohong.The Accuracy Study of Air-to-Air Missile Head Aiming Angles[J].Fire Control & Command Control,1999,24(1):15-19. |
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| Authors: | Zhao Hongliang Mao Shiyi Li Shaohong |
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| Abstract: | The seeker aim angles are two of air to air missile launch and control parameters.Their accuracy is necessary to ensure the seeker lock on the target reliably.The model to compute these parameters is given based on the Lead pursuit attack mode.The uncertainties effect on the seeker aiming parameters due to the airborne radar errors are studied,and the computer simulation structure is established.Then the computation results are given and discussed. |
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| Keywords: | air to air missile missile launch error analysis |
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