2011 IEEE Energy Conversion Congress and Exposition 2011
DOI: 10.1109/ecce.2011.6063852
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A four legs matrix converter based ground power unit with selective harmonic control

Abstract: In this paper a three phase four leg matrix converter is proposed to implement a 400Hz Aircraft Ground Power Supply unit. A parallel structure resonant controller is used to regulate the power supply output voltage providing very good tracking of the output voltage reference even in the presence of a non linear load. Simulations results and experimental validation from a 7.5KVA converter prototype are presented to validate the operation of the proposed converter.

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Cited by 9 publications
(4 citation statements)
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“…To obtain the model of the cell, the switches were considered as ideal. This was possible because the switching frequency was much greater than the modulation frequency [39,40], and with the switching constraint in Equation (2), the system dynamics were only related to the input and output filters. Figure 8 shows the diagram of the electrical equivalent .…”
Section: Stabilitymentioning
confidence: 99%
“…To obtain the model of the cell, the switches were considered as ideal. This was possible because the switching frequency was much greater than the modulation frequency [39,40], and with the switching constraint in Equation (2), the system dynamics were only related to the input and output filters. Figure 8 shows the diagram of the electrical equivalent .…”
Section: Stabilitymentioning
confidence: 99%
“…components with a target settling time of 20 ms. For compensation of -ve seq. components which appear as 2 nd harmonic components in dq, the following resonant controller has been employed [13] …”
Section: Fb Controllermentioning
confidence: 99%
“…The design, as well as the control and implementation of a three-phase GPU for aircraft servicing is presented in [18], [19] using a three-phase matrix converter where an output LC filter is considered at the output side. A four-leg matrix converter with an output LC filter is proposed to be used as a 400[Hz] aircraft ground power unit (AGPU) in [20], [21]. A resonant controller and a single loop repetitive voltage controller are considered to regulate the converter in order to obtain a fixed load frequency and voltage independent of the load present on the aircraft grid using optimal Venturini and SVM techniques.…”
Section: Introductionmentioning
confidence: 99%