[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]

弹箭与制导学报 >

2024 , Vol. 44 >Issue 1: 98 - 102

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2024.01.015

基于L1制导的巡飞弹航迹跟踪技术

  • 王帅为 ,
  • 王荣刚 ,
  • 王嘉文 ,
  • 梁益铭
展开
  • 西安现代控制技术研究所,陕西 西安 710065

王帅为(1992—),男,工程师,硕士,研究方向:导航制导与控制。

收稿日期: 2022-10-25

  网络出版日期: 2024-12-28

收起

Course Tracking Technology of Loitering Missile Based on L1 Guidance

  • WANG Shuaiwei ,
  • WANG Ronggang ,
  • WANG Jiawen ,
  • LIANG Yiming
Expand
  • Xi’an Modern Control Technology Research Institute,Xi’an 710065,Shaanxi, China

Received date: 2022-10-25

  Online published: 2024-12-28

Fold

摘要

针对巡飞弹航迹跟踪问题,基于L1制导律,提出了一种巡飞弹航迹跟踪方法。首先,将航迹跟踪分为圆航迹跟踪和直线航迹跟踪,分别针对初始位置与理论航迹的几何关系,推导了不同状态下前置角的表达式;然后,提出了圆航迹和直线航迹跟踪策略,确保巡飞弹无超调的沿着理论航迹飞行;最后,通过仿真验证,提出的制导策略对圆形航迹与多边形航迹具有良好的跟踪效果,L1训导律比PD控制收敛更快,稳态误差更小。

关键词： L1制导; 巡飞弹; 航迹跟踪

本文引用格式

王帅为 , 王荣刚 , 王嘉文 , 梁益铭 . 基于L1制导的巡飞弹航迹跟踪技术[J]. 弹箭与制导学报, 2024 , 44(1) : 98 -102 . DOI: 10.15892/j.cnki.djzdxb.2024.01.015

Abstract

Based on the L1 guidance law, this paper proposes a track tracking method for loitering missiles. Course tracking is divided into circular course tracking and straight course tracking. According to the geometric relationship between the initial position and the theoretical course, the expressions of the leading angle under different states are derived, and the circular course and straight course tracking strategies are proposed to ensure that the loitering missile can fly along the theoretical course without overshoot. Finally, the simulation results show that the proposed guidance strategy has good tracking effect on circular course and polygonal course.

Key words： L1 guidance law; loitering missile; course tracking

[an error occurred while processing this directive]

参考文献

原文顺序 | 文献年度倒序 | 文中引用次数倒序
[1]
张从泾, 白文华, 郑红生. 智能化弹药巡飞弹最新发展概述及展望[J]. 国防制造技术, 2021(1): 3-7.

ZHANG C J, BAI W H, ZHENG H S. The latest development and prospect of intellingent ammunition curise missile[J]. Defense Mannfacturing Technology, 2021(1): 3-7.

[2]
解广华, 邹丹. 巡飞弹发展看点[J]. 轻兵器, 2014(21): 10-13.

XIE G H, ZOU D. Cruise missile development highlights[J]. Light weapons, 2014(21): 10-13.

[3]
PARK S, DEYST J, HOW J. A new nonlinear guidance logic for trajectory tracking: AIAA 2004-4900[R]. Reston: AIAA, 2004.

[4]
SUJIT P B, SRIKANTH S, SOUSA J. Unmanned aerial vehicle path following: a survey and analysis of algorithms for fixed-wing unmanned aerial vehicles[J]. IEEE Control System Magazine, 2014, 34(1): 42-59.

[5]
ZHANG J, LI Q, CHENG N, et al. Nonlinear path-following method for fixed-wing unmanned aerial vehicles[J]. Journal of Zhejiang University-Science C( Computers & Electronics), 2013, 14 (2) : 125-132.

[6]
ERAN D B M, PETER W G. Synthetic-waypoint guidance algorithm for following a desired flight trajectory[J]. Journal of Guidance Control and Dynamics, 2010, 33(2): 601-606.

[7]
VENKATRAMAN K, MANI V, KOTHARI M, et al. A suboptimal path planning algorithm using rapidly exploring random trees[J]. International Journal of Aerospace Innovations, 2010, 2(1) : 93-104.

[8]
RATNOO A. Adaptive optimal path following for high wind flights[C]// IFAC. Proceedings of the 18th IFAC World Congress. Milano: IFAC, 2011: 12985-12990.

[9]
NELSON D R, BARBER D B, MCLAIN T W, et al. Vector field path following for miniature air vehicles[J]. IEEE Transactions on Robotics, 2007, 23(3): 519-529.

[10]
黄叙磊, 王根, 张宝. 巡飞弹航迹导引方法. 研究[J]. 弹箭与制导学报, 2010, 30(2): 45-48.

HUANG X L, WANG G, ZHANG B. Guidance appwach study for scout missile flight track[J]. Journal of Projectiles, Rockets, Missile and Guidance, 2010, 30(2): 45-48.

[11]
钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学[M]. 北京: 北京理工大学出版社, 2000.

QIAN X F, LIN R X, ZHAO Y N. Missile flight mechanics[M]. Beijing: Beijing University of Technology Press, 2000.

Options
文章导航

/

〈 〉

[an error occurred while processing this directive]