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dc.contributor.authorSingh, Davinder
dc.description.abstractAdvancements in the field of electrical and electronic aircraft technologies have introduced a concept of a ‘More Electric Aircraft’. This concept essentially replaces non-electrical systems on an aircraft such as Hydraulic and Pneumatic systems with electrical systems. This will create an environment with a high density of electrical loads which will require constant monitoring for electrical fault signals and rapid isolation. Advancements in power electronics and digital control systems have led to the exploration of Solid-State Power Controller(SSPC) as a replacement for the electromechanical protection devices. This thesis documents the design, development, and testing of the SSPC control card which integrates power electronics with digital control systems. The control card measurement and isolation control peripherals, design and tests’ results are thoroughly discussed. The design and test results of a protection card are explored to serve the purpose of overvoltage protection for the power semiconductor.en_US
dc.format.extent73 p.en_US
dc.rightsNanyang Technological University
dc.subjectDRNTU::Engineering::Electrical and electronic engineeringen_US
dc.titleDesign and testing of a solid-state power controller control and protection card for aerospace applicationen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorMuhammad Faeyz Karimen_US
dc.contributor.schoolSchool of Electrical and Electronic Engineeringen_US
dc.description.degreeBachelor of Engineering (Electrical and Electronic Engineering)en_US
dc.contributor.researchRolls-Royce@NTU Corporate Lab
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Appears in Collections:EEE Student Reports (FYP/IA/PA/PI)
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