Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/1214
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dc.contributor.authorPattanaik, Sushant Kumar-
dc.contributor.authorMahapatra, K K-
dc.date.accessioned2010-04-01T09:07:18Z-
dc.date.available2010-04-01T09:07:18Z-
dc.date.issued2008-
dc.identifier.citation2nd National Conference on Advances in Energy Conversion Technologies (AECT 2008), April 18-19, 2008en
dc.identifier.urihttp://hdl.handle.net/2080/1214-
dc.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
dc.format.extent317590 bytes-
dc.format.mimetypeapplication/pdf-
dc.language.isoen-
dc.subjectAircraft Systemen
dc.subjectCurrent Initialization Schemeen
dc.subjectSoft-Switching Inverteren
dc.subjectRDCLI (Resonant DC Link Inverter)en
dc.subjectZVS (Zero Voltage Switching)en
dc.titleA Novel Control Strategy for 400 Hz Aircraft Power Supply Using Resonant DC Link Inverteren
dc.typeArticleen
Appears in Collections:Conference Papers

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