DocumentCode :
2617180
Title :
Hardware in the loop emulation of synchronous generators for aircraft power systems
Author :
Griffo, A. ; Drury, D.
Author_Institution :
Dept. of Electr. & Electron. Eng., Univ. of Bristol, Bristol, UK
fYear :
2012
fDate :
16-18 Oct. 2012
Firstpage :
1
Lastpage :
6
Abstract :
Testing a piece of equipment under realistic operating conditions typical of a complex power system such as those for more electric aircraft application requires a significant effort in terms of costs and complexity of the experimental test rig. Significant advantages can be achieved by using the Power Hardware in-the-Loop (HIL) concept whereby the performances of a device under test are evaluated in an emulated environment of the remaining components of a complete system. This paper describes the application of the Power HIL concept to the emulation of a wound field synchronous generator of the type used in aircraft power systems. Modeling assumptions are detailed in the paper together with an experimental procedure for parameter extraction. The emulation is realized by a bespoke three phase MOSFET based inverter with appropriate output filters controlled by an FPGA based solution used for real time emulation.
Keywords :
aircraft power systems; field programmable gate arrays; invertors; power MOSFET; power filters; synchronous generators; FPGA based solution; aircraft power systems; bespoke three phase MOSFET based inverter; complex power system; electric aircraft application; loop emulation; output filters; parameter extraction; power HIL concept; power hardware in-the-loop concept; real time emulation; synchronous generators; Aerospace electronics; Emulation; Stator windings; Transient analysis; Voltage control; Voltage measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Systems for Aircraft, Railway and Ship Propulsion (ESARS), 2012
Conference_Location :
Bologna
ISSN :
2165-9400
Print_ISBN :
978-1-4673-1370-4
Electronic_ISBN :
2165-9400
Type :
conf
DOI :
10.1109/ESARS.2012.6387388
Filename :
6387388
Link To Document :
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