首页> 外文期刊>International journal of aerospace engineering >A Three-Dimensional Cooperative Guidance Law of Multimissile System
【24h】

A Three-Dimensional Cooperative Guidance Law of Multimissile System

机译:多导弹系统的三维协同制导律

获取原文
           

摘要

In order to conduct saturation attacks on a static target, the cooperative guidance problem of multimissile system is researched. A three-dimensional guidance model is built using vector calculation and the classic proportional navigation guidance (PNG) law is extended to three dimensions. Based on this guidance law, a distributed cooperative guidance strategy is proposed and a consensus protocol is designed to coordinate the time-to-go commands of all missiles. Then an expert system, which contains two extreme learning machines (ELM), is developed to regulate the local proportional coefficient of each missile according to the command. All missiles can arrive at the target simultaneously under the assumption that the multimissile network is connected. A simulation scenario is given to demonstrate the validity of the proposed method.
机译:为了对静态目标进行饱和攻击,研究了多导弹系统的协同制导问题。使用矢量计算建立了三维制导模型,经典的比例导航制导(PNG)法则扩展到三个维度。基于该制导律,提出了一种分布式协同制导策略,并设计了一种共识协议来协调所有导弹的准时制。然后,开发了一个包含两个极限学习机(ELM)的专家系统,以根据命令调节每个导弹的局部比例系数。在连接多导弹网络的前提下,所有导弹都可以同时到达目标。仿真结果表明了该方法的有效性。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号