系统工程与电子技术

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考虑飞行初段弹道交叉的多导弹协同发射时序规划方法

张家铭, 刘忠, 石建迈, 陈超, 张明星   

  1. 国防科学技术大学信息系统工程重点实验室, 湖南 长沙 410073
  • 出版日期:2017-01-20 发布日期:2010-01-03

Fire scheduling for multiple missiles cooperative engagement considering trajectory intersection during the initial flight phase

ZHANG Jiaming, LIU Zhong, SHI Jianmai, CHEN Chao, ZHANG Mingxing   

  1. Science and Technology on Information Systems Engineering Laboratory,
    National University of Defense Technology, Changsha 410073, China
  • Online:2017-01-20 Published:2010-01-03

摘要:

在多导弹协同作战条件下,协调不同导弹发射平台之间的导弹发射顺序,避免导弹飞行初段弹道的相互干扰,快速计算所有导弹的发射时间变得十分迫切和异常困难。为解决多导弹协同发射时序规划问题,以最小化完成导弹发射任务的最终时间为优化目标,建立了多导弹发射时序协同规划的混合整数规划模型。设计了快速启发式算法,给出了发射时间求解算法及基于空间压缩思想的可行解进化策略,可辅助指挥员快速生成导弹发射时序方案。以30枚导弹协同发射为案例,对模型和算法进行了仿真验证。实验结果表明,该模型和方法能有效解决多导弹协同发射时序规划问题。

Abstract:

Under the circumstances of multiple missiles cooperative engagement, it is becoming more urgent and difficult to coordinate the sequence of the launching operations and calculate all the missiles’ launch timing fast. In order to solve the problem of scheduling the launch sequential timing of multiple missiles cooperative engagement, a mixed integer programming model of multi-missile and multi-waypoint is built, and the last sequential timing is optimized to the minimum as the objective. A fast heuristic algorithm is designed, which may help commanders provide a launch sequential timing plan with the priority requirement. The method is formulated to handle the trajectory intersection based on time dimension optimization, and the solving algorithm of launch timing and the feasible solution evolution strategy based on space compression are presented. A case study of 30 missiles is used to verify the model and the algorithm. The results show the effectiveness of the proposed method on such a problem.