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Nonlinear disturbance observer enhanced dynamic inversion control of missiles

journal contribution
posted on 2008-10-24, 09:05 authored by Wen-Hua ChenWen-Hua Chen
Nonlinear dynamic inversion control (NDIC) is one of the most promising nonlinear control methods in aerospace engineering. For longitudinal dynamics of a missile, this paper proposes a nonlinear disturbance observer based approach 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.

History

School

  • Aeronautical, Automotive, Chemical and Materials Engineering

Department

  • Aeronautical and Automotive Engineering

Citation

CHEN, W-H., 2003. Nonlinear disturbance observer enhanced dynamic inversion control of missiles. Journal of Guidance, Control and Dynamics, 26 (1), pp.161-166.

Publisher

© American Institute of Aeronautics and Astronautics

Publication date

2003

Notes

This article is Restricted Access. It was published in the journal Journal of guidance, control and dynamics [© American Institute of Aeronautics and Astronautics] and is available at: http://www.aiaa.org/content.cfm?pageid=322&lupubid=23

ISSN

0731-5090

Language

  • en