系统工程与电子技术
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王光辉, 吕超, 谢宇鹏, 刘文超
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WANG Guang-hui, LV Chao, XIE Yu-peng, LIU Wen-chao
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摘要:
针对歼击机机动规避空空导弹问题,建立了一种有导弹制导动力学滞后的空空导弹飞机的追逃运动学二维模型,研究了飞机机动时机、机动方式对主动寻的空空导弹过载需求和脱靶量的影响,并根据机动脱靶量仿真了飞机机动逃逸概率,得到了机动可大幅度提高飞机逃逸概率,开关机动优于圆机动,以及机动周期越短规避效果越好的结论,解决了飞机机动规避空空导弹的定量评价问题。
Abstract:
For the problem of a fighter evasive maneuver of air-to-air missiles, a two-dimensional pursuit-evasion- model of the fighter against air-to-air missiles is built on missile time constant. The effectiveness of the fighter maneuver time and mode on the miss distance and overload requirement of air-to-air missiles is studied. And the evasive probability caused by miss distance, which is produced through fighter maneuver, is calculated. The conclusions that maneuver can increase evasive probability, on-off maneuver is superior to circle maneuver and a shorter maneuver period is better are gotten, which solve the problem of lack a quantity method to evaluate a fighter evasive maneuver air-to-air missiles.
王光辉, 吕超, 谢宇鹏, 刘文超. 歼击机规避空空导弹的评价算法[J]. 系统工程与电子技术, doi: 10.3969/j.issn.1001-506X.2016.11.17.
WANG Guang-hui, LV Chao, XIE Yu-peng, LIU Wen-chao. Evasive maneuver model of a fighter against air-to-air missiles[J]. Systems Engineering and Electronics, doi: 10.3969/j.issn.1001-506X.2016.11.17.
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链接本文: https://www.sys-ele.com/CN/10.3969/j.issn.1001-506X.2016.11.17
https://www.sys-ele.com/CN/Y2016/V38/I11/2561