New Method for Missile Control using Sliding Mode Control

被引：0
|
作者：
Mardani, Mohammad [1 ]
Ghasemi, Ali Reza [1 ]
机构：
[1] Shahab Danesh Univ, Dept Elect Engn, Qom, Iran
来源：
2017 IEEE INTERNATIONAL CONFERENCE ON POWER, CONTROL, SIGNALS AND INSTRUMENTATION ENGINEERING (ICPCSI) | 2017年
关键词：
nonlinear model; non-minimum phase; sliding mode controller; pitch channel; INTEGRATED GUIDANCE;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
A new method is introduced and simulated for control of pursuit missiles The method implements a nonlinear model and a sliding mode controller is designed for the system to cope with unknown parameters such as aerodynamic coefficients and moment of inertia and to make the system robust. Simulation results show satisfactory performance in terms of efficiency and stability for sliding mode controller and optimal behavior when applied to the linear model.
引用
收藏
页码：43 / 48
页数：6
相关论文
共 50 条
  • [1] Supersonic Missile Control with PI Sliding Mode Method
    Ma, Qiang
    Jin, Yuqiang
    [J]. MANUFACTURING SCIENCE AND TECHNOLOGY, PTS 1-3, 2011, 295-297 : 1773 - 1776
  • [2] A new sliding mode control design for integrated missile guidance and control system
    Guo, Jianguo
    Xiong, Yu
    Zhou, Jun
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 78 : 54 - 61
  • [3] Sliding Mode Control for Integrated Missile Guidance and Control System
    Xiong, Yu
    Guo, Jianguo
    Zhou, Jun
    [J]. PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 8371 - 8374
  • [4] Integrated guidance and control of missile based on Nussbaum gain adaptive sliding mode control method
    Qi, Hui
    Zhang, Ze
    Xu, Jiang-Tao
    Han, Peng-Xin
    Zhang, De-Wei
    [J]. Kongzhi yu Juece/Control and Decision, 2017, 32 (01): : 93 - 99
  • [5] Integrated Missile Guidance and Control Using Adaptive Sliding Mode Approach
    Wang Xianghua
    Wang Jinzhi
    [J]. PROCEEDINGS OF THE 31ST CHINESE CONTROL CONFERENCE, 2012, : 4611 - 4616
  • [6] Output Redefinition Method for Sliding Mode Control of Nonminimum Phase Missile Systems
    Parali, Yagiz
    Jafarov, Elbrous M.
    [J]. 2015 7TH INTERNATIONAL CONFERENCE ON RECENT ADVANCES IN SPACE TECHNOLOGIES (RAST), 2015, : 151 - 156
  • [7] Time-varying sliding mode control of missile based on suboptimal method
    Li Zongxing
    Zhang Rui
    [J]. JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2021, 32 (03) : 700 - 710
  • [8] Robust sliding mode control with ESO for dual-control missile
    Shang, Wei
    Tang, Shengjing
    Guo, Jie
    Ma, Yueyue
    Yun, Yuhang
    [J]. JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2016, 27 (05) : 1073 - 1082
  • [9] Robust sliding mode control with ESO for dual-control missile
    Wei Shang
    Shengjing Tang
    Jie Guo
    Yueyue Ma
    Yuhang Yun
    [J]. Journal of Systems Engineering and Electronics, 2016, 27 (05) : 1073 - 1082
  • [10] Time-varying sliding mode control of missile based on suboptimal method
    LI Zongxing
    ZHANG Rui
    [J]. Journal of Systems Engineering and Electronics, 2021, 32 (03) : 700 - 710
12345