Nonlinear disturbance observer-enhanced dynamic inversion control of missiles

被引:467
作者
Chen, WH [1 ]
机构
[1] Loughborough Univ Technol, Loughborough LE11 3TU, Leics, England
关键词
D O I
10.2514/2.5027
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Nonlinear dynamic inversion control (NDIC) is one of the most promising nonlinear control methods in aerospace engineering. For longitudinal dynamics of a missile, a nonlinear disturbance observer-based approach is proposed to enhance its disturbance attenuation ability and performance robustness against uncertain aerodynamic coefficients. Stability of the proposed nonlinear disturbance observer-enhanced NDIC is established. Its flexibility and efficiency are demonstrated by two different choices of the nonlinear gain function in the observer.,Simulation results show that the nonlinear disturbance observer-based technique can significantly improve disturbance attenuation ability and performance robustness of dynamic inversion control.
引用
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页码:161 / 166
页数:6
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