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Application Of Artificial Neural Network in The Performance of Non Linear Twin Rotor Mimo System (Record no. 57760)

MARC details
000 -LEADER
fixed length control field	02102nam a2200169Ia 4500
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	14MPE09
100 ## - MAIN ENTRY--AUTHOR NAME
Personal name	Sara Hafeez Rajput
--	14MPE09
--	Supervisor Prof. Dr. Aslam Pervez Memon
245 #0 - TITLE STATEMENT
Title	Application Of Artificial Neural Network in The Performance of Non Linear Twin Rotor Mimo System
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Place of publication	Nawabshah
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Name of publisher	QUEST
260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT)
Year of publication	2017
300 ## - PHYSICAL DESCRIPTION
Number of Pages	64
500 ## - GENERAL NOTE
General note	ABASTRACT<br/><br/>The control and modeling of flexible maneuvering system, such as helicopter unmanned vehicles has always been a challenging problem due to-linearity, significant cross-coupling between its two, complex aerodynamics force between its two rotors and the of some of its states and outputs for measurements. Helicopter has been widely used in air traffic systems, such as traffic condition assessment, prevention and crime precautions. The twin rotor multiple input multiple output system (TRMS) is a laboratory setup which resemble the behavior of a helicopter in certain aspects due to the complicated nonlinearity and high cross coupling effect between main rotor and tail rotor like helicopter. Some of its inputs and outputs are inaccessible for the measurement. The control effort is to make the beam of TRMS to move quickly and accurately to the desired attitudes both in terms of pitch angle and azimuth angle under decoupling effects between two axes. The project is aimed at devising a model of the non-linear MIMO system by using Neural Networks. This is because of the efficient modeling approach provided by neural networks highly non-non-linear systems. The mathematical modeling of TRMS is done using MATLAB/Simulink. The simulation results are compared with the results of conventional PID controller.<br/>The results of A (MLP & (RBF) show better transient, rise time, overshoot and steady state response as compared to conventional PID controller.<br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/><br/>
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name	Department of Master Engineering in Power Engineering Of Electrical Engineering
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier	http://tiny.cc/cs2cvz
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Koha item type	Thesis and Dissertation

Holdings
Withdrawn status	Lost status	Home library	Current library	Date acquired	Accession Number	Koha item type
		Research Section	Research Section	16/05/2018	MP/17-168	Thesis and Dissertation
		Research Section	Research Section	08/10/2018	MP/30-340	Thesis and Dissertation