| Yang Zhe（杨哲）,Li Shulin,Li Shouan,Zhou Li,Zhang Jun.[J].高技术通讯(英文),2014,20(2):117~123 |
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| Calculation model of military aircraft survivability to a missile |
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| DOI：10.3772/j.issn.1006-6748.2014.02.002 |
| 中文关键词: |
| 英文关键词: survivability, missile, miss distance, Monte Carlo, kill probability |
| 基金项目: |
| Author Name | Affiliation | | Yang Zhe（杨哲） | | | Li Shulin | | | Li Shouan | | | Zhou Li | | | Zhang Jun | |
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| 中文摘要: |
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| 英文摘要: |
| Since missiles are main threat against aircrafts in air war, a model is proposed for calculating the aircraft survivability to a missile. The hit characteristic of aircraft to a missile is analyzed, and then Monte Carlo method is applied to generate missile detonation location according to its distribution rule. In addition, based on the analysis of fragment trajectory and critical components, the intersection point of these two is determined. Then the kill probability of critical component to a fragment can be calculated, and the aircraft survivability to a missile is obtained accordingly. Finally, the feasibility of the proposed method is demonstrated. Simulation results show that this method captures the basic effects of missile detonation locations on aircraft survivability, which may provide an effective reference to aircraft survivability research. |
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