Gain-scheduled bank-to-turn autopilot design using linear parameter varying transformations

被引：0
作者：
Univ of Texas at Austin, Austin, United States [1 ]
机构：
来源：
J Guid Control Dyn | / 5卷 / 1056-1063期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
18
引用
收藏
相关论文
共 50 条
  • [31] Autopilot design for bank-to-turn missiles using receding horizon predictive control scheme
    Seoul Natl Univ, Seoul, Korea, Republic of
    J Guid Control Dyn, 6 (1248-1254):
  • [32] Missile gain-scheduled autopilot design using D-K-D iteration
    Yu, Jian-Qiao
    Wen, Zhong-Hui
    Xu, Cheng-Dong
    Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2009, 26 (08): : 855 - 859
  • [33] Gain-scheduled H∞ filtering of parameter-varying systems
    Zhou, Shaosheng
    Zhang, Baoyong
    Zheng, Wei Xing
    INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 2006, 16 (08) : 397 - 411
  • [34] Gain-scheduled controllers for linear parameter-varying systems with saturating actuators: LMI-based design
    Montagner, Vinicius F.
    Oliveira, Ricardo C. L. F.
    Peres, Pedro L. D.
    Tarbouriech, Sophie
    Queinnec, Isabelle
    2007 AMERICAN CONTROL CONFERENCE, VOLS 1-13, 2007, : 2481 - +
  • [35] Gain-scheduled stabilisation of linear parameter-varying systems with time-varying input delay
    Wang, J.
    Shi, P.
    Gao, H.
    Wang, J.
    IET CONTROL THEORY AND APPLICATIONS, 2007, 1 (05) : 1276 - 1285
  • [36] Comparing linear parameter-varying gain-scheduled control techniques for active flutter suppression
    Barker, JM
    Balas, GJ
    JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2000, 23 (05) : 948 - 955
  • [37] Gain-scheduled H2 control of linear parameter varying systems using a parametric Lyapunov function
    de Souza, CE
    Trofino, A
    2004 43RD IEEE CONFERENCE ON DECISION AND CONTROL (CDC), VOLS 1-5, 2004, : 2936 - 2941
  • [38] Missile H-infinity gain-scheduled autopilot design based on quasi-linear model
    Yu, Jian-Qiao
    Luo, Guan-Chen
    Wen, Zhong-Hui
    Kongzhi Lilun Yu Yingyong/Control Theory and Applications, 2009, 26 (04): : 451 - 454
  • [39] Decoupling design for bank-to-turn missile autopilot using multivariable frequency-domain approach
    Guofang Keji Daxue Xuebao, 6 (13-16):
  • [40] ROBUST ADAPTIVE BANK-TO-TURN MISSILE AUTOPILOT DESIGN USING FUZZY CMAC NEURAL NETWORKS
    张友安
    崔平远
    王守斌
    杨涤
    Chinese Journal of Aeronautics, 1998, (03)
12345