DocumentCode
3102782
Title
Control of a Matrix Converter-based AC Power Supply for Aircrafts under Unbalanced Conditions
Author
Arévalo, Saúl López ; Zanchetta, Pericle ; Wheeler, Patrick W.
Author_Institution
Univ. of Nottingham, Nottingham
fYear
2007
fDate
5-8 Nov. 2007
Firstpage
1823
Lastpage
1828
Abstract
This paper deals with the design, control and implementation of a 10 kVA three-phase ground power supply unit (GPU) for aircraft servicing. Instead of a classical back to back converter configuration, a 3-phase to 3-phase direct AC-AC (matrix) converter has been used as the power conditioning core of the power supply, working in conjunction with input and output LC filters. An optimized control system in the ABC frame employing a repetitive controller has been successfully implemented taking into account both the transient and steady state performance targets together with the system effectiveness under extreme unbalanced conditions. Extensive simulations prove the efficiency of the designed system in meeting the international standards requirements.
Keywords
AC-AC power convertors; aircraft control; aircraft power systems; matrix convertors; optimal control; predictive control; AC power supply; aircraft servicing; direct AC-AC converter; matrix converter; optimized control system; output LC filters; repetitive controller; three-phase ground power supply unit; Aerospace control; Aerospace electronics; Aircraft propulsion; Bandwidth; Control systems; Matrix converters; Military aircraft; Power supplies; Switching frequency; Voltage control;
fLanguage
English
Publisher
ieee
Conference_Titel
Industrial Electronics Society, 2007. IECON 2007. 33rd Annual Conference of the IEEE
Conference_Location
Taipei
ISSN
1553-572X
Print_ISBN
1-4244-0783-4
Type
conf
DOI
10.1109/IECON.2007.4460406
Filename
4460406
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