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An online-implementable differential evolution tuned all-aspect guidance law

机译:可在线执行的差分进化调整的全方位指导律

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摘要

This paper proposes a differential evolution based method of improving the performance of conventional guidance laws at high heading errors, without resorting to techniques from optimal control theory, which are complicated and suffer from several limitations. The basic guidance law is augmented with a term that is a polynomial function of the heading error. The values of the coefficients of the polynomial are found by applying the differential evolution algorithm. The results are compared with the basic guidance law, and the all-aspect proportional navigation laws in the literature. A scheme for online implementation of the proposed law for application in practice is also given.
机译:本文提出了一种基于差分进化的方法,该方法在高航向误差下可提高常规制导律的性能,而无需借助来自最优控制理论的技术,该技术既复杂又受若干限制。基本航向定律用航向误差的多项式函数来扩充。多项式系数的值是通过应用差分进化算法找到的。将结果与基本制导律和文献中的全方面比例导航律进行比较。还给出了在线实施拟议法律以在实践中应用的方案。

著录项

  • 来源
    《Control Engineering Practice》 |2010年第10期|p.1197-1210|共14页
  • 作者

    T. Raghunathan; D. Ghose;

  • 作者单位

    Guidance, Control and Decision Systems Laboratory, Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India;

    Guidance, Control and Decision Systems Laboratory, Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    missile guidance; optimal control; genetic algorithm; online control; real-time;

    机译:导弹制导;最佳控制;遗传算法在线控制;即时的;

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