| 大气参数偏差对再入弹头爆点射程的影响 |
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| 引用本文： | 王明海,赵久奋.大气参数偏差对再入弹头爆点射程的影响[J].飞行力学,1998,16(3):93-96. |
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| 作者姓名： | 王明海 赵久奋 |
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| 作者单位： | 西安第二炮兵工程学院 |
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| 摘 要： | 统计出了实际大气状态参数与标准大气状态参数的最大偏差值，以等高程和等过载引信两种弹头引信方式建立了大气参数偏差对弹道式导弹弹头引爆点射程影响的数学模型，从理论上分析了大气参数偏差对弹道式导弹弹头引爆点对应射程产生影响的物理实质；进而以一种洲际弹道导弹为例，讨论出大气参数偏差引起弹头命中点射程偏差的具体数值。
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| 关 键 词： | 大气参数 再入弹头 射程偏差 弹道导弹 |
Research on Effect of Atmosphere Parameter Error on Range of Reentry Warhead Explosion Spot |
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| Wang Minghai,Zhao Jiufen,Kang Jianbin.Research on Effect of Atmosphere Parameter Error on Range of Reentry Warhead Explosion Spot[J].Flight Dynamics,1998,16(3):93-96. |
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| Authors: | Wang Minghai Zhao Jiufen Kang Jianbin |
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| Institution: | The Second Artillery Engineering College |
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| Abstract: | On the basis of statistics of the deviation maximum between the actual atmosphere parameter and standard atmosphere parameter.A mathematical model is established solely according to two kinds of warhead fuze modes considering that atmosphere parameter error works on the flight of warhead explosion spot of ballistic missile. Then, a physics essence's theoretical analysis about this influence is provided out. Finally, a calculation example on intercontinental ballistic missile is presented. What's more, the concrete numerical value that the atmosphere parameter error leads to the range deviation is worked out. |
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| Keywords: | Atmosphere parameter Reentry warhead Range deviation |
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