Nonlinear Adaptive Control Design for Ship-to-Ship Missiles

被引:3
作者
Im, Ki Hong [1 ]
机构
[1] Samsung Elect Co, Suwon, Gyeonggi Do, South Korea
关键词
Adaptive; autopilot; nonlinear; STT missiles;
D O I
10.1007/s12555-013-0383-3
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Ship-to-ship missiles have relatively large weight and complex cross couplings between each channel and, practically, the aerodynamic uncertainties also make it difficult to analyze and control it. In this paper, an approximate missile model is presented with parametric affine structure applicable to all operating points. An approximate minimum phase dynamics is also derived. The uncertainties in aerodynamic forces are modeled into parametric form to design a nonlinear adaptive controller.
引用
收藏
页码:1118 / 1123
页数:6
相关论文
共 5 条
  • [1] Design of a missile autopilot using adaptive nonlinear dynamic inversion
    Hindman, R
    Shell, WM
    [J]. ACC: PROCEEDINGS OF THE 2005 AMERICAN CONTROL CONFERENCE, VOLS 1-7, 2005, : 327 - 332
  • [2] Im KH, 2006, INT J CONTROL AUTOM, V4, P255
  • [3] Lee C., 2012, P INT C AER SCI ICAS
  • [4] 한광호, 2011, International Journal of Aeronautical and Space Sciences, V12, P78
  • [5] [No title captured]