Arc fault protection for more electric aircraft application by Neppalli Sri Chandra Pranavi

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Topologies and control methods for protection of DC electrical system in aircraft by Marwaha, Mridul

“…Conventional aircraft are evolving towards more-electric aircraft, replacing the mechanical, pneumatic, and hydraulic subsystems with their electrical counterparts. …”
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Control algorithm for embedded machine for hostile environment by Lee, Jun Jie

“…With the increase advancement of more electric aircraft, much research has been done for the optimization of the aircraft engine. …”
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Solid state power controller by Ng, Tze Wei

“…The advancement of technology in the field of electrical and electronics engineering has introduced a concept and developing pattern for All-Electric and More-Electric Aircraft (MEA/AEA) system and design. A MEA has significant advantages over a conventional mechanical system in its weight, cost, and space. …”
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Development of electrical machines for hostile environment by Wang, Shuai

“…This thesis focuses on improving the electromagnetic performance of switched reluctance machines (SRM) without compromising their mechanical advantages to fulfil the demanding requirements of more-electric aircraft. Literature review reveals the advantages of sinusoidal excited mutually coupled (MC) SRM windings in boosting the power density and reducing the torque ripple. …”
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The Vienna rectifier in aircraft applications: current distortion mitigation methods by Anushka, Molligoda Liyanage Devinda

“…Electrical power demand is steadily increasing in more electric aircraft (MEA) as conventional pneumatic, hydraulic and mechanical loads are being replaced by electrical loads. …”
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Development of DC/AC power controller in aerospace power system by Ang, Cheryl Hui Miin

“…More aircraft are adopting the More Electrical Aircraft (MEA) concept, which aims to drive the aircraft subsystem with more electrical power. …”
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