Intelligent control of twin-rotor MIMO system using fuzzy inference techniques
The flight control system of helicopter is difficult to control for their performance of high-order unstable, nonlinear, and multiple-inputs multiple-outputs (MIMO) system. The behavior of two degree-of-freedom (2-DOF) helicopter has significant cross-coupling between pitch and yaw directional motio...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Praise Worthy Prize
2013
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| Online Access: | http://psasir.upm.edu.my/id/eprint/28559/1/Intelligent%20Control%20of%20Twin.pdf |