基于改进烟花算法的空战指挥引导对策生成  

Generation of air combat command and guidance countermeasures based on improved fireworks algorithm

作　　者：余敏建[1] 游航航 韩其松[1] 杨海燕[1] 高阳阳 YU Minjian;YOU Hanghang;HAN Qisong;YANG Haiyan;GAO Yangyang(Air Traffic Control And Navigation College, Air Force Engineering University, Xi’an 710051, China;Graduate College, Air Force Engineering University, Xi’an 710051, China;Unit 93175 of the PLA, Changchun 130000, China)

机构地区：[1]空军工程大学空管领航学院,陕西西安710051 [2]空军工程大学研究生院,陕西西安710051 [3]中国人民解放军93175部队,吉林长春130000

出　　处：《系统工程与电子技术》2019年第12期2780-2788,共9页Systems Engineering and Electronics

基　　金：国家自然科学基金(61472441);装备预研领域基金(61403110304);空军工程大学校长基金(XZJY2018031)资助课题

摘　　要：针对新型空战条件下指挥引导对策生成问题,提出了一种基于改进烟花算法的指挥引导对策生成方法。首先分析了现有模型的不足,在综合考虑角度、距离、速度、高度态势以及战机性能的基础上,构建并加入支援保障因素模型,构造指挥引导对策生成综合指标函数;其次针对传统自适应烟花算法在收敛精度和速度方面的不足,将轮盘赌选择、维度方差、禁忌搜索思想用于改进其中的变异算子和选择算子;最后针对改进的模型和算法进行了仿真分析。仿真结果表明,改进的模型更加符合实际,算法的收敛精度、收敛速度更优,对于解决空战指挥引导对策生成问题具有更好的效果。Aiming at the problem of command and guidance countermeasure generation under new air combat conditions, a command and guidance countermeasure generation method based on the improved fireworks algorithm is proposed. Firstly, the shortcomings of the existing models are analyzed, and a support factor model is built and added. Then, considering the advantages and threats of angle, distance, speed and height, as well as the performance factors of fighter planes, a comprehensive index function is constructed. Finally, aiming at the shortcomings of the traditional adaptive fireworks algorithm in convergence accuracy and convergence speed, roulette wheel selection, dimensional variance and tabu search are applied to improving mutation operator and selection operator, and simulation analysis is carried out for the improved algorithm. The simulation results show that the improved model is more practical, the convergence accuracy and convergence speed of the algorithm are better, and it has better effect on solving the problem of air combat command and guidance countermeasure generation.

关 键 词：空战 烟花算法 指挥引导 支援保障 轮盘赌 维度方差 禁忌搜索 

分 类 号：V249[航空宇航科学与技术—飞行器设计]