Geodesic
Tracking Control Algorithms for a Laboratory Aerodynamical System
International Journal of Applied Mathematics and Computer Science, Tome 14 (2004) no. 4, pp. 469-475.

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The tracking control problem of a strongly nonlinear MIMO system is presented. The system shares some features with a helicopter, such as important interactions between the vertical and horizontal motions. The dedicated I/O board allows for control, measurements and communication with a PC. The RTWT toolbox in the MATLAB environment is used to perform real-time experiments. The control task is to track a predefined reference trajectory. A mathematical model of the system, containing experimental characteristics, is used to design the controllers: a multidimensional PD, a suboptimal controller in the sense of a quadratic performance index and a variable gain controller.
Keywords: nonlinear systems, real-time control, tracking control, suboptimal controller
Mots-clés : system nieliniowy, sterowanie w czasie rzeczywistym, sterowanie nadążne, kontroler suboptymalny 
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Gorczyca, P.; Hajduk, K. Tracking Control Algorithms for a Laboratory Aerodynamical System. International Journal of Applied Mathematics and Computer Science, Tome 14 (2004) no. 4, pp. 469-475. http://geodesic.mathdoc.fr/item/IJAMCS_2004_14_4_a3/

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