系统工程与电子技术

• 制导、导航与控制 • 上一篇    下一篇

基于遗传算法的卫星攻击轨道优化方法

赵琳, 李玉玲, 刘源, 郝勇, 王艺鹏   

  1. 哈尔滨工程大学自动化学院, 黑龙江 哈尔滨 150001
  • 出版日期:2016-04-25 发布日期:2010-01-03

Optimization method research of satellite attaching track#br# planning based on genetic algorithm

ZHAO Lin, LI Yu-ling, LIU Yuan, HAO Yong, WANG Yi-peng   

  1. College of Automation, Harbin Engineering University, Harbin 150001, China
  • Online:2016-04-25 Published:2010-01-03

摘要:

在空间攻防与卫星对抗中,当目标卫星周围有若干小卫星以编队形式对其绕飞时,为使拦截卫星成功击中目标卫星,并且避开编队小卫星的防御区,必须对拦截卫星攻击轨道进行规划。寻找到一条既能满足安全性、快速性,又能节省燃料的最优路径。而利用经典数学规划方法,如序列二次规划方法,虽能寻找到最优路径,但并不适应于解决空间对抗中复杂攻防环境模型下的轨道规划问题。为此本文提出基于遗传算法的拦截卫星攻击轨道寻优方法。建立目标卫星编队小卫星的动态防御模型作为环境模型,采用可变长度实数编码方式,根据攻击轨道安全性、快速性、燃料消耗最少等要求建立综合适应度函数,并对遗传算子及置换运算方法进行设计。通过仿真验证,本文提出的轨道优化方法能够寻求到最优攻击路径,并且算法收敛速度较快。

Abstract:

In the warfare of antisatellite, when formation micro-satellite is flying around the target satellite, in order to avoid the defensive area of microsatellite, it is needed to find a track security track which needs less fuel. A method to find the best attacking track based on the genetic algorithm is proposed. The dynamic defensive model of the target micro-satellite is built as the environment model, using variable length encoding real numbers. Establish the comprehensive fitness function based on security, rapidity and fuel, and design the selection operator, crossover operator, mutation operator and replacement calculation method. Numerical simulations show that the proposed method can get the best attacking track, and have a faster convergence rate.