Transactions of Nanjing University of Aeronautics & Astronautics
Normal
Dynamic Surface Control with Nonlinear Disturbance Observer for Uncertain Flight Dynamic System
- Article
- Figures
- Metrics
- Preview PDF
- Reference
- Related
- Cited by
- Materials
Abstract:
A new robust control method of a nonlinear flight dynamic system with aerodynamic coefficients and external disturbance has been proposed. The proposed control system is a combination of the dynamic surface control (DSC) and the nonlinear disturbance observer (NDO). DSC technique provides the ability to overcome the “explosion of complexity” problem in backstepping control. NDO is adopted to observe the uncertainties in nonlinear flight dynamic system. It has been proved that the proposed design method can guarantee uniformly ultimately boundedness of all the signals in the closed-loop system by Lyapunov stability theorem. Finally, simulation results show that the proposed controller provides better performance than the traditional nonlinear controller.
Keywords:
Project Supported:
Clc Number:
Mobile website
