摘要
在拦截弹推进系统和弹道参数的设计中 ,引入多目标多约束的模糊优化方法 ,在约束条件一定的情况下 ,合理选择和分配几个重要的设计变量 ,使得拦截弹的总质量最小、拦截时间最短。
During the design of propulsion system and trajectory parameters,the multi objectives and multi restrictions fuzzy optimization is used to solve the problem of how we can choose and distribute the important design variables to minimize interceptor′s total mass and flight time,under the condition that restrictions are given.
出处
《现代防御技术》
2002年第4期28-31,共4页
Modern Defence Technology
