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Controller design for a twin rotor helicopter model via exact state feedback linearization

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2 Author(s)
Mustafa, G. ; Dept. of Electr. Eng., Pakistan Inst. of Eng. & Appl. Sci., Islamabad, Pakistan ; Iqbal, N.

Controller design via feedback linearization of the plant is a powerful approach to some of the nonlinear control problems. This paper presents the feedback linearization of a twin rotor helicopter model. Twin rotor system is a two input two output nonlinear system. The task is to control the angular position of the system. A state feedback controller is designed based on the resulting linear system. The effectiveness of the approach is shown by simulations.

Published in:

Multitopic Conference, 2004. Proceedings of INMIC 2004. 8th International

Date of Conference:

24-26 Dec. 2004