Robust adaptive control of nonlinear system based on QFT application to 3DOF flight control system /

This research is a development of a hybrid controller design constructed by robust and adaptive controller application to three degree of freedom (3 DOF) helicopter flight control model. 3 DOF helicopter model is a lab developed benchmark model of actual helicopter with operation of nonlinearities,...

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Bibliographic Details
Main Author: Boby, Rounakul Islam (Author)
Format: Thesis
Language:English
Published: Kuala Lumpur : Kulliyyah of Engineering, International Islamic University Malaysia, 2017
Subjects:
Online Access:http://studentrepo.iium.edu.my/handle/123456789/5190
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