[an error occurred while processing this directive] [an error occurred while processing this directive] [an error occurred while processing this directive]
[an error occurred while processing this directive]

一种带攻击角度约束的快速收敛无抖振制导律设计

  • 吕梅柏 ,
  • 高环 ,
  • 任子薇
展开
  • 1 西北工业大学宇航学院, 西安 710072
    2 航天飞行动力学技术重点实验室, 西安 710072
    3 海军驻20所军事代表室, 西安 710068
    4 西安现代控制技术研究所, 西安 710065

吕梅柏(1982-), 男, 副教授, 博士, 研究方向: 导航、制导与控制技术研究。

收稿日期: 2017-09-25

  网络出版日期: 2025-05-28

Design of a Fast Convergent Chattering-free Guidance LawWith Attack Angle Constraint

  • LYU Meibo ,
  • GAO Huan ,
  • REN Ziwei
Expand
  • 1 School of Astronautics, Northwestern Polytechnical University, Xi'an 710072, China
    2 National Key Laboratory of Aerospace Flight Dynamics, Xi'an 710072, China
    3 Military Representative Office of Navy in No. 20 Research Institute, Xi'an 710068, China
    4 Xi'an Modern Control Technology Research Institute, Xi'an 710065, China

Received date: 2017-09-25

  Online published: 2025-05-28

摘要

针对小型战术导弹以一定角度攻击目标的问题,文中提出了一种基于观测器的有限时间收敛制导律。利用非齐次干扰观测器对系统未知扰动进行估计,避免了制导律可能带来的抖振问题,采用幂次自适应趋近律,使得视线角及视线角速度在该制导律下能够快速的收敛至期望值,同时满足脱靶量和攻击角度约束要求,相比于传统制导律,具有一定的优越性。数值仿真结果表明了该方法的有效性。

本文引用格式

吕梅柏 , 高环 , 任子薇 . 一种带攻击角度约束的快速收敛无抖振制导律设计[J]. 弹箭与制导学报, 2018 , 38(1) : 97 -100,104 . DOI: 10.15892/j.cnki.djzdxb.2018.01.023

Abstract

In order to solve the problem that small tactical missile attacked targets at a certain angle, a finite time convergent guidance law based on observer was proposed in this paper. The nonhomogeneous disturbance observer was employed to estimate the unknown disturbance of the system, which avoid the chattering that may caused by guidance law. A power adaptive reaching law was applied to make the LOS and LOS speed converge to the expected value rapidly, at the same time, it met the requirements of miss distance and attack angle constraint. Compared with the traditional guidance law, it has some advantages. And the numerical simulation results demonstrate the effectiveness of the proposed method.

[an error occurred while processing this directive]

参考文献

[1]
SHE H P, YANG S X, NI H, et al. A Nonlinear Optimal Guidance Law with Terminal Impact Angle Constraint [J]. International Journal of Computational Intelligence Systems, 2011, 4(6): 1319-1324.
[2]
KUMAR S R, RAO S, GHOSE D. Nonsingular terminal sliding mode guidance with impact angle constraints [J]. Journal of Guidance, Control, and Dynamics, 2014, 37(4): 1114-1130.
[3]
张运喜, 孙明玮, 陈增强. 滑模变结构有限时间收敛制导律 [J]. 控制理论与应用, 2012, 29(11): 1413-1418.
[4]
黄洁, 张友安, 刘永新. 一种有撞击角和视场角约束的运动目标的偏置比例导引算法 [J]. 宇航学报, 2016, 37(2): 195-202.
[5]
王颖, 宋龙, 张拥军. 制导滑翔炸弹的最优末制导律研究 [J]. 弹箭与制导学报, 2010, 30(4): 51-54.
[6]
孙胜, 周荻. 有限时间收敛变结构导引律 [J]. 宇航学报, 2008, 29(4): 1258-1262.
[7]
周慧波, 宋申民, 宋俊红. 基于观测器的有限时间收敛的滑模导引律设计 [J]. 中南大学学报(自然科学版), 2016, 47(1): 91-99.
文章导航

/

[an error occurred while processing this directive]