This thesis proposes new power converter topologies suitable for
aircraft systems. It also proposes both AC-DC and DC-DC types of
converters for different electrical loads to improve the
performance these systems. To increase fuel efficiency and reduce
environmental impacts, less efficient non-electrical aircraft
systems are being replaced by electrical systems. However, more
electrical systems requires more electrical power to be generated
in the aircraft. The increased consumption of electrical power in
both civil and military aircrafts has necessitated the use of more
efficient electrical power conversion technologies. This book
presents acomprehensive mathematical analysis and the design and
digital simulation of the power converters. Subsequently it
discusses the construction of the hardware prototypes of each
converter and the experimental tests carried out to verify the
benefits of the proposed solutions in comparison to the existing
solutions.
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