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dc.contributor.authorPattanaik, Sushant Kumar-
dc.contributor.authorMahapatra, K K-
dc.identifier.citationIEEE Sponsored Conference on Computational Intelligence, Control And Computer Vision In Robotics & Automation, CICCRA 2008, March 10-11, 2008en
dc.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
dc.format.extent162146 bytes-
dc.subjectAircraft System,en
dc.subjectSoft-Switching Inverter,en
dc.subjectPWM (Pulse Width Modulation),en
dc.subjectZVS (Zero Voltage Switching),en
dc.subjectRDCLI (Resonant DC Link Inverter).en
dc.titleAircraft Power Supply Design using Soft-Switched Inverteren
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