479.575 PEOPLE
People | Locations | Statistics |
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Ziakopoulos, Apostolos | Athens |
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Vigliani, Alessandro | Turin |
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Catani, Jacopo | Rome |
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Statheros, Thomas | Stevenage |
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Utriainen, Roni | Tampere |
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Guglieri, Giorgio | Turin |
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Martínez Sánchez, Joaquín |
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Tobolar, Jakub |
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Volodarets, M. |
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Piwowar, Piotr |
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Tennoy, Aud | Oslo |
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Matos, Ana Rita |
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Cicevic, Svetlana |
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Sommer, Carsten | Kassel |
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Liu, Meiqi |
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Pirdavani, Ali | Hasselt |
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Niklaß, Malte |
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Lima, Pedro | Braga |
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Turunen, Anu W. |
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Antunes, Carlos Henggeler |
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Krasnov, Oleg A. |
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Lopes, Joao P. |
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Turan, Osman |
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Lučanin, Vojkan | Belgrade |
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Tanaskovic, Jovan |
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Wheeler, P.
in Cooperation with on an Cooperation-Score of 37%
Topics
- aircraft
- design
- electronic equipment
- electronics
- reliability
- voltage
- inverter
- driveline
- modeling
- rectifier
- autotransformer
- generator
- theory
- electric power
- stability analysis
- bus
- engine
- inductive interference
- civil aircraft
- synchronous motor
- minimisation
- takeoff
- duct
- topology
- assessment
- performance evaluation
- variable
- filter
- modernization
- actuating system
- actuator
- simulation
- icing
- deicing
- rudder
- motor
- permanent magnet
- show 7 more
Publications (32/32 displayed)
- 2021Optimal and automated decentralised converter control design in more electrical aircraft power electronics embedded grids
- 2020Reliability oriented thermal management of aircraft power converters
- 2019Wide Bandgap Voltage Source Inverter Design for Automotive Electric Drivetrain
- 2018Generic functional modelling of multi-pulse auto-transformer rectifier units for more-electric aircraft applicationscitations
- 2018Development of Aircraft Electric Starter-Generator System Based-On Active Rectification Technologycitations
- 2017Control Design and Voltage Stability Analysis of a Droop-Controlled Electrical Power System for More Electric Aircraftcitations
- 2017Thermal Design of Linear Induction and Synchronous Motors for Electromagnetic Launch of Civil Aircraftcitations
- 2016The importance of load pulse timing in aircraft generationcitations
- 2016Minimization of electro-mechanical interaction with posicast strategies for more-electric aircraft applicationscitations
- 2016An Improved Voltage Compensation Approach in a Droop-Controlled DC Power System for the More Electric Aircraftcitations
- 2016Superconducting Electromagnetic Launch System for Civil Aircraftcitations
- 2016Superconducting and conventional electromagnetic launch system for civil aircraft assisted take-offcitations
- 2015Impact of Electric Loads on Engine Shaft Dynamics within More Electric Aircraftcitations
- 2015Electromagnetic launch systems for civil aircraft assisted take-offcitations
- 2014DC side ripple cancellation in a cascaded multi-level topology for automotive applicationscitations
- 2014Power conversion for a novel AC/DC aircraft electrical distribution systemcitations
- 2014An optimized bi-directional, wide speed range electric starter-generator for aerospace applicationcitations
- 2014The more electric aircraft: Technology and challengescitations
- 2014Stability of multi-source droop-controlled Electrical Power System for more-electric aircraftcitations
- 2013Performance evaluation of 3-phase buck-type PWM rectifiers with integratted and symmetrical Boost converter using SiC MOSFETS for aircraft applicationcitations
- 2013Optimal LCL filter design for 3-phase Space Vector PWM rectifiers on variable frequency aircraft power systemcitations
- 2012Regeneration of energy onto an aircraft electrical power system from an electro-mechanical actuatorcitations
- 2011Power flow analysis in electro-mechanical actuators for civil aircraftcitations
- 2011Advanced techniques for accelerated simulation studies of complex aircraft electrical power systemscitations
- 2010Design of an expulsive de-icing system for avionic applications: Preliminary study and functional tests
- 2009Performance evaluation of two stagematrix converters for EMA in aircraft applicationscitations
- 2008Regeneration in aircraft electrical power systems?citations
- 2008Fast reduced functional models of electromechanical actuators for more-electric aircraft power system studycitations
- 2008Performance assessment of matrix converter and two stage matrix converter for EMA in aircraft applicationcitations
- 2005A 20 KW matrix converter drive system for an Electro-Mechanical Aircraft (EMA) actuator
- 2004Dynamic performance of a matrix converter driven electro-mechanical actuator for an aircraft rudder
- 2003A matrix converter based permanent magnet motor drive for an aircraft actuation systemcitations
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