Aircraft Power Supply Design using Soft-Switched Inverter

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

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DC Field	Value	Language
dc.contributor.author	Pattanaik, Sushant Kumar	-
dc.contributor.author	Mahapatra, K K	-
dc.date.accessioned	2010-03-26T11:57:51Z	-
dc.date.available	2010-03-26T11:57:51Z	-
dc.date.issued	2008	-
dc.identifier.citation	IEEE Sponsored Conference on Computational Intelligence, Control And Computer Vision In Robotics & Automation, CICCRA 2008, March 10-11, 2008	en
dc.identifier.uri	http://hdl.handle.net/2080/1210	-
dc.description.abstract	This 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
dc.format.extent	162146 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.subject	Aircraft System,	en
dc.subject	Soft-Switching Inverter,	en
dc.subject	PWM (Pulse Width Modulation),	en
dc.subject	ZVS (Zero Voltage Switching),	en
dc.subject	RDCLI (Resonant DC Link Inverter).	en
dc.title	Aircraft Power Supply Design using Soft-Switched Inverter	en
dc.type	Article	en
Appears in Collections:	Conference Papers

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