A Novel Control Circuit for Aircraft Power Supply Using Soft-Switched Inverter

Please use this identifier to cite or link to this item: http://hdl.handle.net/2080/927

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DC Field	Value	Language
dc.contributor.author	Pattanaik, Sushant Kumar	-
dc.contributor.author	Mahapatra, K K	-
dc.date.accessioned	2009-07-25T12:02:35Z	-
dc.date.available	2009-07-25T12:02:35Z	-
dc.date.issued	2009	-
dc.identifier.citation	IEEE International Conference on Industrial Technology. ICIT 2009,Gippsland, VIC, 10-13 February, 1-6 Pages.	en
dc.identifier.uri	http://dx.doi.org/10.1109/ICIT.2009.4939721	-
dc.identifier.uri	http://hdl.handle.net/2080/927	-
dc.description.abstract	This paper describes the design of a novel aircraft power supply. Power supply design is designed using a softswitched Resonant DC Link Inverter (RDCLI). A current initialization scheme based on state transition equation is adopted to avoid zero crossing failures. Zero-hysteresis bangbang control is used for current control within the inverter. The designed power supply supports 400 Hz load. The advantages of the power supply design using soft-switched inverter rather than conventional hard switched PWM inverter in terms of adequate current regulator bandwidth and reduced switching losses are brought out. The proposed solution is validated through extensive MATLAB and CASPOC simulation.	en
dc.format.extent	790689 bytes	-
dc.format.mimetype	application/pdf	-
dc.language.iso	en	-
dc.publisher	IEE	en
dc.subject	aircraft power systems	en
dc.subject	electric current control	en
dc.subject	power supply circuits	en
dc.subject	resonant invertors	en
dc.title	A Novel Control Circuit for Aircraft Power Supply Using Soft-Switched Inverter	en
dc.type	Article	en
Appears in Collections:	Conference Papers

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