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弹箭与制导学报 >

2011 , Vol. 31 >Issue 3: 6 - 10

DOI: https://doi.org/10.15892/j.cnki.djzdxb.2011.03.007

导弹与制导技术

基于滑模控制的导弹制导控制一体化设计

  • 苗昊春 ,
  • 马清华 ,
  • 陈韵 ,
  • 程冬
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  • 1 清华大学自动化系,北京 100084
    2 中国兵器工业第203研究所,西安 710065

苗吴春(1986-),男,内蒙古赤峰人,硕士研究生,研究方向:导弹制导控制一体化设计。

收稿日期: 2010-10-22

  网络出版日期: 2025-05-30

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Integrated Design of Missile Guidance and Control Based on Sliding-mode Control

  • MIAO Haochun ,
  • MA Qinghua ,
  • CHEN Yun ,
  • CHENG Dong
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  • 1 Department of Automation, Tsinghua University, Beijing 100084, China
    2 No.203 Research Institute of China Ordance Industries, Xi'an 710065, China

Received date: 2010-10-22

  Online published: 2025-05-30

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摘要

文中对某滚转稳定反坦克导弹的俯仰和偏航通道建立了制导控制一体化数学模型,在末制导段分别采用经典方法和一体化方法设计了滑模制导律(SMG)和自适应滑模一体化制导控制律(SMGC),建立了基于dSPACE的半实物仿真系统,并对两种制导律进行了数字和半实物仿真,结果表明:一体化方法优于传统方法,可有效提高导弹制导性能。

关键词： 滑模控制; 制导控制一体化; dSPACE; 半实物仿真

本文引用格式

苗昊春 , 马清华 , 陈韵 , 程冬 . 基于滑模控制的导弹制导控制一体化设计[J]. 弹箭与制导学报, 2011 , 31(3) : 6 -10 . DOI: 10.15892/j.cnki.djzdxb.2011.03.007

Abstract

Integrated guidance and control models in pitch and yaw channels were built on a roll stable anti tank missile in this paper. Conventional and integrated methods were used respectively to design the sliding mode guidance (SMG) law and the integrated guidance and control of adaptive sliding mode (SMGC) in the terminal guidance session. The hardware-in-the-loop based on dSPACE was established and the SMG and SMGC laws were simulated. The results indicate that the integrated method is better than the conventional and the guidance performance has been proved effectively.

Key words： sliding mode control; integrated guidance and control; dSPACE; hardware-in-the-loop

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参考文献

[1]
魏毅寅, 梁冰, 谭峰,等. 导弹俯仰通道制导与控制一体化设计[J]. 黑龙江大学自然科学学报, 2007, 24(4): 14-18.
[2]
程继红. 飞行器控制导引一体化设计方法研究[J]. 海军航空工程学院学报, 2006, 21(2): 227-230.
[3]
Menon P K, Ohlmeyer E J. Integrated design of agile missile guidance and autopilot systems[J]. Control Engineering Practice, 2001, 9(10): 1095-1106.
[4]
周狄. 寻的新型导引规律[M]. 北京: 国防工业出版社, 2002.
[5]
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.
[6]
谭乐祖, 李大鹏, 何金新. 舰空导弹制导与控制一体化三维模型建立[J]. 弹箭与制导学报, 2010, 30(1): 7-9.
[7]
张保群, 宋申民. 基于自适应滑模的导弹制导与控制一体化反演设计[J]. 弹箭与制导学报, 2009, 29(5): 31-35.
[8]
吴进华, 刘洪兴, 史贤俊. dSPACE仿真平台的实时仿真原理研究及其应用[J]. 电子测量与仪器学报, 2004(增刊): 720-724.
[9]
马培蓓, 吴进华, 纪军. dSPACE 实时仿真平台软件环境及应用[J]. 系统仿真学报, 2004, 16(4): 667-670.
[10]
SPACE. Installation and Configuration Reference For Release 3.5[Z]. 2003.
[11]
雷叶红, 张记华, 张春明. 基于 dSPACE/MATLAB/Simulink 平台的实时仿真技术研究[J]. 系统仿真技术, 2005, 17(3): 131-135.
[12]
dSPACE. Experiment Guide for Release 3.5[Z]. 2003.
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