The Optimal Attitude Controller Design and Simulation of Three-Axis Dual Rotor Helicopter

Abstract:

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In this paper, the model of three-axis dual rotor helicopter is built, through a new motor control algorithm of real-time grouping, the decoupling and independent control of pitch, yaw and roll channels is realized; then the “dead zone” is introduced to design the attitude controller on the basis of the optimal control law which minimize the weighted sum of response time and energy consumption, to achieve optimal control of the attitude of the helicopter; finally, the simulation model of the attitude control system is established in the MATLAB/Simulink environment. Simulation results show the feasibility of the optimal attitude controller design.

Info:

Periodical:

Edited by:

Zhixiang Hou

Pages:

1265-1268

DOI:

10.4028/www.scientific.net/AMM.128-129.1265

Citation:

C. Z. Xu and T. Zhang, "The Optimal Attitude Controller Design and Simulation of Three-Axis Dual Rotor Helicopter", Applied Mechanics and Materials, Vols. 128-129, pp. 1265-1268, 2012

Online since:

October 2011

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Price:

$35.00

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