Non-linear modeling and PID control of twin rotor MIMO system

This paper deals with PID control tuning for a nonlinear multi-input multi-output system (MIMO). In this paper, a laboratory helicopter model called the twin rotor MIMO system (TRMS) is considered as a MIMO system. The mathematical modeling of helicopter model is simulated using MATLAB/Simulink for...

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Bibliographic Details
Published in2012 IEEE International Conference on Advanced Communication Control and Computing Technologies pp. 366 - 369
Main Authors Ramalakshmi, A. P. S., Manoharan, P. S.
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.08.2012
Subjects
Mathematical model
MATLAB
MIMO
Multi-input multi-output (MIMO)
proportional-integral-derivative (PID)
twin rotor MIMO system (TRMS)
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ISBN1467320455
9781467320450
DOI10.1109/ICACCCT.2012.6320804

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Summary:This paper deals with PID control tuning for a nonlinear multi-input multi-output system (MIMO). In this paper, a laboratory helicopter model called the twin rotor MIMO system (TRMS) is considered as a MIMO system. The mathematical modeling of helicopter model is simulated using MATLAB/Simulink for controlling it. The two degrees of freedom (2-DOF) are controlled both in horizontal and vertical direction using proportional-integral-derivative (PID) controller. Simulation results are obtained for different input signals. Moreover the error of the plant output and control output of PID controller are presented which show the performance evaluation of TRMS.
ISBN:1467320455
9781467320450
DOI:10.1109/ICACCCT.2012.6320804