Abstract
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.
Original language | English |
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Pages (from-to) | 161-166 |
Number of pages | 6 |
Journal | Journal of Guidance, Control, and Dynamics |
Volume | 26 |
Issue number | 1 |
DOIs | |
Publication status | Published - 2003 |
ASJC Scopus subject areas
- Control and Systems Engineering
- Aerospace Engineering
- Space and Planetary Science
- Electrical and Electronic Engineering
- Applied Mathematics