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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/1214

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contributor.authorPattanaik, Sushant Kumar-
contributor.authorMahapatra, K K-
date.accessioned2010-04-01T09:07:18Z-
date.available2010-04-01T09:07:18Z-
date.issued2008-
identifier.citation2nd National Conference on Advances in Energy Conversion Technologies (AECT 2008), April 18-19, 2008en
identifier.urihttp://hdl.handle.net/2080/1214-
description.abstractThis paper presents the control aspects in designing an aircraft power supply. Power supply design is done using a soft-switched Resonant DC Link Inverter (RDCLI). A novel current initialization scheme is adopted to avoid zero crossing failures. Zero-hysteresis bang-bang control is used for current control within the inverter. The power supply is designed for 400 Hz load. The soft-switched inverter provides adequate current regulator bandwidth besides reducing switching losses. The proposed solution is validated through extensive simulation.en
format.extent317590 bytes-
format.mimetypeapplication/pdf-
language.isoen-
subjectAircraft Systemen
subjectCurrent Initialization Schemeen
subjectSoft-Switching Inverteren
subjectRDCLI (Resonant DC Link Inverter)en
subjectZVS (Zero Voltage Switching)en
titleA Novel Control Strategy for 400 Hz Aircraft Power Supply Using Resonant DC Link Inverteren
typeArticleen
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