| 引用本文: | 张为华,方丁酉,张育林.一种固体导弹最大射程评定方法.[J].国防科技大学学报,1999,21(1):13-16.[点击复制] |
| Zhang Weihua,Fang Dingyou,Zhang YuLing.Maximum Range Evaluation Method for Solid Missiles[J].Journal of National University of Defense Technology,1999,21(1):13-16[点击复制] |
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| 一种固体导弹最大射程评定方法 |
| 张为华, 方丁酉, 张育林 |
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(国防科技大学 航天技术系 湖南 长沙 410073)
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| 摘要: |
| 本文提出了一种基于固体火箭发动机性能散布分析的固体导弹最大射程评定方法, 将系统辨识、性能散布分析和统计分析有机结合, 实用性强, 对固体导弹试验鉴定技术研究具有重要意义。 |
| 关键词: 固体导弹, 射程, 评定方法 |
| DOI： |
| 投稿日期：1998-09-28 |
| 基金项目: |
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| Maximum Range Evaluation Method for Solid Missiles |
| Zhang Weihua, Fang Dingyou, Zhang YuLing |
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(Department of Aerospace Technology, NUDT, Changsha, 410073)
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| Abstract: |
| in this paper, the maximum range evaluation method for solid missiles based on solid rocket motor performance dispersion analysis is presented. The method is the combination of system identification, performance dispersion analysis for solid rocket motor and range statistic analysis, which is practical and significant for solid missiles flight test qualification. |
| Keywords: solid missiles, maximum range, evaluation method |
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