HP nonlinear guidance law design based on smooth sliding mode control

被引：0
|
作者：
Ge, Lian-Zheng [1 ]
Shen, Yi [1 ]
Xu, Guang-Chi [1 ]
机构：
[1] Dept. of Control Science and Engineering, Harbin Institute of Technology, Harbin 150001, China
来源：
Journal of Harbin Institute of Technology (New Series) | 2009年 / 16卷 / 03期
关键词：
Aerodynamics;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
下载
收藏
页码：382 / 385
相关论文
共 50 条
  • [31] The Design of Finite-time Convergence Guidance Law for Head Pursuit based on Adaptive Sliding Mode Control
    Zhang, Cheng
    Zhang, Ke
    Wang, Jingyu
    ICINCO: PROCEEDINGS OF THE 13TH INTERNATIONAL CONFERENCE ON INFORMATICS IN CONTROL, AUTOMATION AND ROBOTICS, VOL 2, 2016, : 110 - 118
  • [32] Design of Guidance Law Based on Nonsingular Terminal Sliding Mode Control and Finite-time Disturbance Observer
    Jin, Shi
    Zhang, Zhenxing
    Li, Shihua
    2014 13TH INTERNATIONAL WORKSHOP ON VARIABLE STRUCTURE SYSTEMS (VSS), 2014,
  • [33] Designing integrated guidance and control law for air to air missile based on sliding mode control
    Zhu, Zhanxia
    Chen, Peng
    Tang, Biwei
    Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, 2014, 32 (02): : 213 - 219
  • [34] Sliding-mode-control-based Differential Geometric Guidance Law using Mild Sliding Manifolds
    Huang, Jingshuai
    Zhang, Hongbo
    Lv, Wei
    Tang, Guojian
    Bao, Weimin
    2018 CHINESE AUTOMATION CONGRESS (CAC), 2018, : 105 - 110
  • [35] Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control
    School of Automation Science and Electrical Engineering, Beihang University, Beijing
    100191, China
    不详
    100191, China
    Wang, Qing (wangqing@buaa.edu.cn), 1600, Chinese Journal of Aeronautics (27):
  • [36] Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control
    Ran Maopeng
    Wang Qing
    Hou Delong
    Dong Chaoyang
    Chinese Journal of Aeronautics, 2014, (03) : 634 - 642
  • [37] Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control
    Ran Maopeng
    Wang Qing
    Hou Delong
    Dong Chaoyang
    Chinese Journal of Aeronautics, 2014, 27 (03) : 634 - 642
  • [38] Backstepping design of missile guidance and control based on adaptive fuzzy sliding mode control
    Ran Maopeng
    Wang Qing
    Hou Delong
    Dong Chaoyang
    CHINESE JOURNAL OF AERONAUTICS, 2014, 27 (03) : 634 - 642
  • [39] Design of stochastic sliding mode variable structure guidance law based on adaptive EKF
    Hui, Zhao
    Jun, Liu Wan
    Hui, Yang Jin
    Bo, Xuan Yong
    PEEA 2011, 2011, 23
  • [40] Design of 3-Dimensional Discrete Sliding Mode Guidance Law Based on ESO
    Wen Nuan
    Liu Zhenghua
    Chang Le
    PROCEEDINGS OF THE 2015 INTERNATIONAL CONFERENCE ON ELECTROMECHANICAL CONTROL TECHNOLOGY AND TRANSPORTATION, 2015, 41 : 14 - 17
12345