more-electric aircraft
Advanced Technological Solutions of Key Components of Variable Frequency of Power Supply System ASE of Modern Aircraft in Accordance with the Concept of a More Electric Aircraft MEA
6
Silicon carbide MOSFETs in more electric aircraft power converters: the performance and reliability benefits over silicon IGBTs for a specified flight mission profile
10
Modal analysis of a PMSG based DC electrical power system in the more electric aircraft using eigenvalues sensitivity
11
Minimization of electro mechanical interaction with posicast strategies for more electric aircraft applications
6
Improving the operating efficiency of the more electric aircraft concept through optimised flight procedures
17
Stability assessment of a droop controlled multi generator electrical power system in the more electric aircraft using parameter space approach
8
Application of Model Detection Techniques to Health Monitoring for the Electrical Network of More Electric Aircraft
6
More electric aircraft starter generator system with utilization of hybrid modulated model predictive control
6
Active front end rectifier modelling using dynamic phasors for more electric aircraft applications
24
Generic functional modelling of multi pulse auto transformer rectifier units for more electric aircraft applications
9
High Efficiency and High Speed PM Motors for the More Electric Aircraft
10
Comparison of two three phase pll systems for more electric aircraft
11
Multi port power conversion systems for the more electric aircraft
6
A smart transformer rectifier unit for the more electric aircraft
5
The impact of impulsive voltage waveforms on the electrical insulation of actuators for more electrical aircraft (MEA)
5
Preliminary noise assessment of aircraft with distributed electric propulsion
22
Hybrid electric aircraft propulsion case study for skydiving mission
22
Noise assessment of aircraft with distributed electric propulsion using a new noise estimation framework
9
Electrical model of carbon fibre reinforced polymers for the development of electrical protection systems for more-electric aircraft
10
Application of SMES-FCL in electric aircraft for stability improvement
6