Title :
Orbit control for a power generating airfoil based on nonlinear MPC
Author :
Gros, Sebastien ; Zanon, Mario ; Diehl, Moritz
Author_Institution :
Optimization in Eng. Center (OPTEC), K.U. Leuven, Leuven, Belgium
Abstract :
The Airborne Wind Energy paradigm proposes to generate energy by flying a tethered airfoil across the wind flow. An essential problem posed by Airborne Wind Energy is the control of the tethered airfoil trajectory during power generation. Tethered flight is a fast, strongly nonlinear, unstable and constrained process, motivating control approaches based on fast Nonlinear Model Predictive Control. In this paper, a computationally efficient 6-DOF control model for a high performance, large-scale, rigid airfoil is proposed. A control scheme based on receding-horizon Nonlinear Model Predictive Control to track reference trajectories is applied to the proposed model. In order to make a real-time application of Nonlinear Model Predictive Control possible, a Real-Time Iteration scheme is proposed and its performance investigated.
Keywords :
aerodynamics; aerospace components; aerospace control; iterative methods; predictive control; wind power; 6-DOF control model; airborne wind energy paradigm; motivating control; nonlinear MPC; nonlinear model predictive control; orbit control; power generating airfoil; real-time iteration scheme; wind flow; Atmospheric modeling; Automotive components; Drag; Process control; Trajectory; Vectors; Wind speed; Optimal Control; Real-time iteration; fast NMPC; flight control; trajectory tracking;
Conference_Titel :
American Control Conference (ACC), 2012
Conference_Location :
Montreal, QC
Print_ISBN :
978-1-4577-1095-7
Electronic_ISBN :
0743-1619
DOI :
10.1109/ACC.2012.6315367