Simulation Of A Matrix Converter Controller, Electro Mechanical Actuator-EMA (For Realistic Operation Condition)

Md Hairul Nizam , Talib (2005) Simulation Of A Matrix Converter Controller, Electro Mechanical Actuator-EMA (For Realistic Operation Condition). Masters thesis, University of Nottingham.

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Abstract

This dissertation describes design and simulation of a matrix converter controller, Electro Mechanical Actuator (EMA) for aircraft. The implementation of the position control in the aircraft actuators system required an accurate, stable and precise output response. The matrix converter is used to control the speed of a permanent magnet motor that determines the position the electro mechanical system (EMA). A correct derivation of mathematical modal of permanent magnet synchronous motor (PMSM) vector controlled is very important and as fundamental of all analysis. In order to design a stable position loop, the fast and stable inner loop control need to be achieved first, followed by the outer loop control for speed and position. In order to have low percent overshoot of the response, the adjustment gain PI controller method is used. Implementing this method, a good response with zero steady state error will be achieved. Analysis of the output simulation response is performed to verify the quality of the design and present in this dissertation.

Item Type: Thesis (Masters)
Uncontrolled Keywords: Actuators -- Design and construction, Air planes -- Control systems
Subjects: T Technology > T Technology (General)
T Technology > TL Motor vehicles. Aeronautics. Astronautics
Divisions: Library > Tesis > FKE
Depositing User: Siti Syahirah Ab Rahim
Date Deposited: 05 Nov 2014 09:04
Last Modified: 28 May 2015 04:29
URI: http://eprints.utem.edu.my/id/eprint/13021
Statistic Details: View Download Statistic

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