DocumentCode :
3110746
Title :
Nonlinear trajectory tracking controller design for flight control with disturbance rejection capability
Author :
Qi, Wang ; Wenhai, Wu ; Li, Xu
Author_Institution :
Naval Aeronaut. Eng. Inst., Qingdao, China
fYear :
2012
fDate :
5-8 Aug. 2012
Firstpage :
162
Lastpage :
167
Abstract :
This article presents the equation of motion for the aircraft in the turbulence. Based on these equations, a trajectory tracking controller is designed using the nonlinear dynamic inverse. In order to reject the disturbance influence, the nonlinear disturbance observer is compensated for the design of the trajectory tracking controller. Simulation results show that the trajectory tracking controller with the nonlinear disturbance observer has a better control performance.
Keywords :
aircraft control; compensation; nonlinear control systems; nonlinear dynamical systems; observers; trajectory control; aircraft; control performance; design compensation; disturbance influence; disturbance rejection capability; equation of motion; flight control; nonlinear disturbance observer; nonlinear dynamic inverse; nonlinear trajectory tracking controller design; turbulence; Aerospace control; Aircraft; Equations; Mathematical model; Observers; Tracking; Trajectory; flight control; nonlinear disturbance observer; unmanned air vehicle;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Mechatronics and Automation (ICMA), 2012 International Conference on
Conference_Location :
Chengdu
Print_ISBN :
978-1-4673-1275-2
Type :
conf
DOI :
10.1109/ICMA.2012.6282835
Filename :
6282835
Link To Document :
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