Terminal sliding mode robust control for swing nozzle

被引：0
|
作者：
机构：
[1] [1,Wang, Wei-Hong
[2] 1,Sun, Liang-Hua
[3] Zhang, Wu-Long
来源：
Zhang, W.-L. | 1600年 / Editorial Department of Electric Machines and Control卷 / 18期
关键词：
Robust control;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [41] On Quantisation of Nonsingular Terminal Sliding Mode Control
    Yan, Y.
    Yu, X.
    Yu, S.
    IFAC PAPERSONLINE, 2023, 56 (02): : 779 - 784
  • [42] A fuzzy terminal sliding mode control method
    Wang, Jun
    2009 WASE INTERNATIONAL CONFERENCE ON INFORMATION ENGINEERING, ICIE 2009, VOL II, 2009, : 293 - 296
  • [43] Terminal sliding mode control for rigid robots
    Tang, Y
    AUTOMATICA, 1998, 34 (01) : 51 - 56
  • [44] Terminal sliding mode control for aeroelastic systems
    Chieh-Li Chen
    Chung-Wei Chang
    Her-Terng Yau
    Nonlinear Dynamics, 2012, 70 : 2015 - 2026
  • [45] Dynamic Behavior of Terminal Sliding Mode Control
    Mu, Chaoxu
    He, Haibo
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2018, 65 (04) : 3480 - 3490
  • [46] Terminal Sliding Mode Attitude Control for Satellite
    Ma, Guangfu
    Lv, Yueyong
    Hu, Qinglei
    Li, Chuanjiang
    2010 8TH WORLD CONGRESS ON INTELLIGENT CONTROL AND AUTOMATION (WCICA), 2010, : 3372 - 3376
  • [47] Terminal Sliding Mode Control of a Boost Converter
    Xu, Meimei
    Ma, Li
    Ding, Shihong
    PROCEEDINGS OF THE 2015 CHINESE INTELLIGENT SYSTEMS CONFERENCE, VOL 2, 2016, 360 : 25 - 33
  • [48] Terminal sliding mode control for rigid robots
    Natl Univ of Mexico, Mexico, Mexico
    Automatica, 1 (51-56):
  • [49] Terminal sliding mode control for aeroelastic systems
    Chen, Chieh-Li
    Chang, Chung-Wei
    Yau, Her-Terng
    NONLINEAR DYNAMICS, 2012, 70 (03) : 2015 - 2026
  • [50] Research of a fuzzy global sliding mode control scheme: A stability control scheme for anti-aircraft missile with swing nozzle thrust vector control
    Liu, Xiaodong
    Zhang, Yu
    Huang, Wanwei
    Wang, Jianmin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2015, 229 (03) : 554 - 561
12345