| 制导精度评定的蒙特卡罗模拟 |
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| 引用本文： | 吴立人. 制导精度评定的蒙特卡罗模拟[J]. 导弹与航天运载技术, 1995, 0(5): 9-17 |
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| 作者姓名： | 吴立人 |
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| 作者单位： | 北京航天自动控制研究所 |
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| 摘 要： | 为解决由于战略导弹飞行试验发数少，难以评定制导精度的困难，开展制导精度评定的蒙特卡罗模拟是必要。本文介绍了战略导弹制导精度评定的蒙特卡罗模拟方法，在工程应用中遇到的几个重要问题以及解决问题的具体方法。
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| 关 键 词： | 战略导弹 制导误差 蒙特卡罗法 数学模型 |
A Monte Carlo Simulation of Guidance Accuracy Evaluation |
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| Wu Liren. A Monte Carlo Simulation of Guidance Accuracy Evaluation[J]. Missiles and Space Vehicles, 1995, 0(5): 9-17 |
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| Authors: | Wu Liren |
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| Affiliation: | Beijing Aerospace Automatic Control Institute |
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| Abstract: | it is necessary to carry out a Monte Carlo simulation of guidance accuracy evaluation in order to solve the problem of evaluating guidance accuracy because of few strategic missile flight tests.A Monte Carlo simulation method of strategic missile guidance accuracy evaluation,several important problems involved in engineering application and specific methods to solve the above problems are introduced. |
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| Keywords: | Strategic missile Guidance error Monte Carlo method Mathematical model. |
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