Title :
Position control by feedback linearization for a simplified helicopter model
Author :
Rebeschieß, Sven ; Roloff, Marc
Author_Institution :
Dept. of Electr. Eng., Tech. Univ. Berlin, Germany
Abstract :
In this paper we describe a method for angular pitch control with feedback linearization for a laboratory helicopter model. Linear angular control can only be applied in a small angle interval. Better control can be obtained by using a linearizing transformation. This transformation tends to be very complex. For the application in this paper it can be shown that a simplified transformation can be sufficient for achieving good control results
Keywords :
attitude control; feedback; helicopters; linearisation techniques; angular pitch control; feedback linearization; linear angular control; linearizing transformation; position control; simplified helicopter model; small angle interval; Control systems; DC motors; Eigenvalues and eigenfunctions; Equations; Helicopters; Laboratories; Linear feedback control systems; Position control; Propellers; Torque control;
Conference_Titel :
Control Applications, 1999. Proceedings of the 1999 IEEE International Conference on
Conference_Location :
Kohala Coast, HI
Print_ISBN :
0-7803-5446-X
DOI :
10.1109/CCA.1999.806165
