A new sliding mode control design for integrated missile guidance and control system

被引：71
|
作者：
Guo, Jianguo [1 ]
Xiong, Yu [1 ]
Zhou, Jun [1 ]
机构：
[1] Northwestern Polytech Univ, Inst Precis Guidance & Control, Xian 710072, Shaanxi, Peoples R China
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2018年 / 78卷
关键词：
Integrated guidance and control (IGC); Sliding mode control; Mismatched uncertainties; Disturbance observer; Lyapunov stability theory; DUAL-CONTROL MISSILES;
D O I：
10.1016/j.ast.2018.03.042
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A new sliding mode control algorithm for integrated guidance and control (IGC) system is proposed in this paper. Firstly, the IGC model is established and the nonlinearities, target maneuvers, perturbations caused by variations of aerodynamic parameters, etc. are viewed as disturbance, so that the IGC system becomes a mismatched uncertain linear system. Secondly, a second-order disturbance observer is used to estimate the disturbances and their derivatives. Thirdly, an integral sliding mode surface is designed to obtain the rudder deflection command directly instead of the back-stepping control (BC) algorithm used in conventional IGC system, which achieves the real sense of IGC, and the stability of the system is proven strictly by Lyapunov stability theory. Finally, the superiority of the proposed IGC method is verified by comparing the simulation results of different methods under different cases. (C) 2018 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码：54 / 61
页数：8
相关论文
共 50 条
  • [1] Sliding Mode Control for Integrated Missile Guidance and Control System
    Xiong, Yu
    Guo, Jianguo
    Zhou, Jun
    PROCEEDINGS OF THE 38TH CHINESE CONTROL CONFERENCE (CCC), 2019, : 8371 - 8374
  • [2] Integrated Missile Guidance and Control Design with Smooth Adaptive Sliding Mode Control
    Zhou Jialing
    Yang Jianying
    2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015, : 5206 - 5211
  • [3] Sliding-mode control for integrated missile autopilot guidance
    Shima, T
    Idan, M
    Golan, OM
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2006, 29 (02) : 250 - 260
  • [4] Integrated guidance and control backstepping design of blended control missile based on adaptive fuzzy sliding mode control
    Wang, Zhao-Lei
    Wang, Qing
    Ran, Mao-Peng
    Dong, Chao-Yang
    Binggong Xuebao/Acta Armamentarii, 2015, 36 (01): : 78 - 86
  • [5] Integrated guidance and control design for missile with terminal impact angle constraint based on sliding mode control
    Peng Wu* and Ming Yang Control and Simulation Center
    Journal of Systems Engineering and Electronics, 2010, 21 (04) : 623 - 628
  • [6] Integrated guidance and control design for missile with terminal impact angle constraint based on sliding mode control
    Wu, Peng
    Yang, Ming
    JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2010, 21 (04) : 623 - 628
  • [7] Integrated design of missile guidance and control based on adaptive back-stepping sliding mode control
    Zhang, Dewei
    Qi, Hui
    Xu, Jiangtao
    Yang, Ya
    Fu, Bangsheng
    An, Tianyu
    PROCEEDINGS OF 2020 3RD INTERNATIONAL CONFERENCE ON UNMANNED SYSTEMS (ICUS), 2020, : 298 - 302
  • [8] Integrated Missile Guidance and Control Using Adaptive Sliding Mode Approach
    Wang Xianghua
    Wang Jinzhi
    PROCEEDINGS OF THE 31ST CHINESE CONTROL CONFERENCE, 2012, : 4611 - 4616
  • [9] Integrated sliding mode guidance and control for a missile with on-off actuators
    Koren, Amir
    Idan, Moshe
    Golan, Oded M.
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2008, 31 (01) : 204 - 214
  • [10] Chattering-free discrete-time sliding mode control for integrated missile guidance and control system
    Wang, Xinming
    Wu, Di
    He, Jingang
    Zhang, Jinpeng
    Li, Shihua
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (07) : 1546 - 1556
12345