Decoupling system design based on variable structure system for BTT missile

被引：0
|
作者：
Tong, Chun-Xia [1 ,2 ]
Wang, Zheng-Jie [2 ]
Zhang, Tian-Qiao [2 ]
机构：
[1] Beijing Institute of Control Engineering, Beijing 100080, China
[2] Department of Mechanism and Control Engineering, Beijing Institute of Technology, Beijing 100081, China
来源：
Yuhang Xuebao/Journal of Astronautics | 2006年 / 27卷 / 01期
关键词：
5;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：27 / 30
相关论文
共 50 条
  • [31] The design of sliding mode control system based on backstepping theory for BTT UAV
    School of Astronautics, Northwestern Polytechnical University, Xi'an, Shaanxi 710072, China
    不详
    不详
    Control Intell Syst, 2008, 4 (347-354):
  • [32] Design of online state monitoring system of certain missile based on embedded system
    Xie Jianhua
    Hao Yongsheng
    Ma Jian
    Yu Haiquan
    ICEMI 2007: PROCEEDINGS OF 2007 8TH INTERNATIONAL CONFERENCE ON ELECTRONIC MEASUREMENT & INSTRUMENTS, VOL I, 2007, : 901 - 903
  • [33] THE DESIGN OF SLIDING MODE CONTROL SYSTEM BASED ON BACKSTEPPING THEORY FOR BTT UAV
    Yao, J.
    Zhu, X.
    Zhou, Z.
    CONTROL AND INTELLIGENT SYSTEMS, 2008, 36 (04)
  • [34] Optimized design of control system based on dynamic soft variable structure
    Li, Feng-Xiang
    Yuan, Ye
    Tien Tzu Hsueh Pao/Acta Electronica Sinica, 2013, 41 (05): : 1025 - 1029
  • [35] Design of neural-adaptive nonlinear autopilot for BTT missile
    Huang, Shu-Cai
    Li, Wei-Min
    Yuhang Xuebao/Journal of Astronautics, 2007, 28 (05): : 1231 - 1234
  • [36] Design method of variable structure control system
    Liu, X.-D., 1600, Editorial Department of Electric Machines and Control (17):
  • [37] The Robust Adaptive Dynamic Surface Controller Design for BTT Missile
    Tang Zhili
    Zhu Yongwen
    2013 32ND CHINESE CONTROL CONFERENCE (CCC), 2013, : 871 - 877
  • [38] Robust Controller Design for BTT Missile Equipped with Grid Fin
    Xu Zhaoqing
    Pei Hailong
    PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 10561 - 10566
  • [39] Design of variable structure control law of a guidance missile
    Wang, Q
    Meng, XY
    ISTM/2003: 5TH INTERNATIONAL SYMPOSIUM ON TEST AND MEASUREMENT, VOLS 1-6, CONFERENCE PROCEEDINGS, 2003, : 1223 - 1226
  • [40] Variable structure controller design with application to missile tracking
    Bhat, MS
    Bai, DS
    Powly, AA
    Swamy, KN
    Ghose, D
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2001, 24 (04) : 859 - 862
12345