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Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/1210

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contributor.authorPattanaik, Sushant Kumar-
contributor.authorMahapatra, K K-
date.accessioned2010-03-26T11:57:51Z-
date.available2010-03-26T11:57:51Z-
date.issued2008-
identifier.citationIEEE Sponsored Conference on Computational Intelligence, Control And Computer Vision In Robotics & Automation, CICCRA 2008, March 10-11, 2008en
identifier.urihttp://hdl.handle.net/2080/1210-
description.abstractThis paper describes the design of an aircraft power supply. Power supply design is done using a softswitched 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 designed power supply supports 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.extent162146 bytes-
format.mimetypeapplication/pdf-
language.isoen-
subjectAircraft System,en
subjectSoft-Switching Inverter,en
subjectPWM (Pulse Width Modulation),en
subjectZVS (Zero Voltage Switching),en
subjectRDCLI (Resonant DC Link Inverter).en
titleAircraft Power Supply Design using Soft-Switched Inverteren
typeArticleen
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