摘要
基于飞机地面压力加油系统管路模型,本文采用高级遗传算法(RGA)的排序选择及随机交换算法,在满足管路最大冲击压力及满油时间差的约束条件下,经全局搜索优化策略,得到优化后适应度最佳的节流孔径,试验研究的结果验证了该方法的可行性和有效性。
Based on the pipeline model of airplane pressure fueling system, the methods of sequential search and random crossover which belong to Refine Genetic Algorithm are presented in this article. On the constraints of fueling time disparity and maximum pulsating pressure, the most appropriate throttle diameter are attained. test results show that the optimal strategy mentioned above is valid and feasible.
出处
《机床与液压》
北大核心
2002年第4期51-52,154,共3页
Machine Tool & Hydraulics
