现代防御技术 ›› 2018, Vol. 46 ›› Issue (6): 44-50.DOI: 10.3969/j.issn.1009-086x.2018.06.007

• 导航、制导与控制 • 上一篇    下一篇

控制量权重可变的主动段最优中制导律

马自茹1, 2, 3 , 魏明英1, 李运迁1   

  1. 1. 北京电子工程总体研究所, 北京 100854;
    2. 中国航天科工集团有限公司 第二研究院, 北京 100854;
    3. 空天防御创新中心, 北京 100854
  • 出版日期:2018-11-30 发布日期:2020-10-22
  • 作者简介:马自茹(1992-), 男, 黑龙江绥化人。硕士生, 主要从事导弹制导控制方面的研究。通信地址:100039 北京市142信箱30分箱 E-mail:15045684858@163.com

Active Section Optimal Midcourse Guidance Law with Controlled Amount Variable Weights

MA Zi-ru1, 2, 3, WEI Ming-ying1, LI Yun-qian1   

  1. 1.Beijing Institute of Electronic Engineering, Beijing 100854, China;
    2.The Second Research Academy of CASIC, Beijing 100854, China;
    3.Air and Space Defense Innovation Center, Beijing 100854, China
  • Online:2018-11-30 Published:2020-10-22

摘要: 在末段高层拦截弹的主动段中制导中, 考虑主动段飞行中导弹的速度的变化, 满足末速度的角度约束, 同时要求使控制量尽可能小, 为了能够实现这些约束, 在指标函数中, 采用时变的控制量权重系数, 利用极小值原理, 伪控制量的办法, 得到了一种最优中制导律。仿真结果表明, 这种指标函数中加入可变控制量权重的办法, 在保证精度的同时, 可以有效地控制控制量的大小。

关键词: 末段高层, 角度约束, 主动段, 可变权重, 最优控制, 极小值原理

Abstract: Considering the change of the velocity of missile in the active section flight in the guidance of the active section of the terminal high altitude interceptor, the angle constraint of the final velocity was required to meet and the control amount was required as small as possible. To realize these constraints, in the index function, an optimal guidance law by adopting the time varying control weight coefficient was obtained, using the minimum principle, as well as pseudo control method. The simulation results showed that the method of adding variable weight in this index function can control the size of the control while guaranteeing the precision.

Key words: end high-level, angle constraint, active section, variable weight, optimal control, minimum principle

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