@inproceedings{f8c1dd99e4404aeaae3dab66ec22aba9,
title = "Comparison and choice of a fault tolerant inverter topology for the traction drive of an electrical helicopter",
abstract = "This paper presents the results of a system analysis of different options for electric inverters for the traction drive of an electrical helicopter. The article explains the optimal choice, in terms of the design requirements and future operation conditions, and the type and topology of electric inverter, to supply the traction permanent magnet synchronous motor from the batteries. The main focus has been given to the study of reliability and fault tolerance of the electric energy inverter. In order to estimate these parameters, the Markov models of the multi-state system reliability evaluation were used.",
keywords = "electrical helicopter, fault tolerance, inverter topology, multilevel inverter, reliability, traction drive",
author = "Igor Bolvashenkov and J{\"o}rg Kammermann and Taha Lahlou and Herzog, {Hans Georg}",
note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016 ; Conference date: 02-11-2016 Through 04-11-2016",
year = "2016",
doi = "10.1109/ESARS-ITEC.2016.7841328",
language = "English",
series = "2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
booktitle = "2016 International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles and International Transportation Electrification Conference, ESARS-ITEC 2016",
}