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基于零控脱靶量的拦截器轨控发动机优化设计
引用本文:齐照辉,梁伟,刘雪梅,翟丽丽,高兰.基于零控脱靶量的拦截器轨控发动机优化设计[J].航空动力学报,2011,26(7):1654-1658.
作者姓名:齐照辉  梁伟  刘雪梅  翟丽丽  高兰
作者单位:航天飞行器生存技术与效能评估实验室,北京,100085
摘    要:为提高动能拦截器变轨拦截能力,考虑目标与拦截器相对距离、相对速度等因素,构建了拦截器零控脱靶量、轨控发动机内弹道、发动机质量与尺寸等优化模型,将遗传算法和Powell算法相结合进行轨控发动机不确定性优化设计.应用算例表明,采用优化设计后的轨控发动机,拦截器可修正的最大零控脱靶量至少提高17.9%,不确定性因素的影响更加...

关 键 词:拦截器  轨控发动机  优化设计  不确定性  零控脱靶量
收稿时间:2010/5/12 0:00:00
修稿时间:2011/1/23 0:00:00

Optimization design of trajectory-control engine of interceptor based on zero-effort-miss
QI Zhao-hui,LIANG Wei,LIU Xue-mei,ZHAI Li-li and GAO Lan.Optimization design of trajectory-control engine of interceptor based on zero-effort-miss[J].Journal of Aerospace Power,2011,26(7):1654-1658.
Authors:QI Zhao-hui  LIANG Wei  LIU Xue-mei  ZHAI Li-li and GAO Lan
Institution:The Institute of Effectiveness Evaluation of Flying Vehicle,Beijing 100085,China;The Institute of Effectiveness Evaluation of Flying Vehicle,Beijing 100085,China;The Institute of Effectiveness Evaluation of Flying Vehicle,Beijing 100085,China;The Institute of Effectiveness Evaluation of Flying Vehicle,Beijing 100085,China;The Institute of Effectiveness Evaluation of Flying Vehicle,Beijing 100085,China
Abstract:To improve the transport and intercepting capability of interceptor considering the relative distance and velocity between target and interceptor, etc, the zero-effort-miss model of interceptor, the internal ballistic model and the mass & size model of trajectory-control engine were established to optimize the trajectory-control engine. The genetic arithmetic combined with Powell method was also adopted in the optimization design of trajectory-control engine. The zero-effort-miss eliminated by trajectory-control engine could improve not less than 17.9% as proved by the optimization design case, and the influence caused by uncertain factors was more explicit, so the method might be applied to the optimization design of interceptor.
Keywords:interceptor  trajectory-control engine  optimization design  uncertainty  zero-effort-miss
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