Comparison and Analysis of Multi-State Reliability of Fault-Tolerant Inverter Topologies for the Electric Aircraft Propulsion System
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Publisher
IEEE
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http://xplorestaging.ieee.org/ielx7/9634173/9634161/09634654.pdf?arnumber=9634654
Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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2. Review, Comprehensive Analysis and Derivation of Analytical Power Loss Calculation Equations for Two- to Three-Level Midpoint Clamped Inverter Topologies with Hybrid Switch Configurations;Energies;2023-09-19
3. Inverter design for future electrified aircraft propulsion systems under consideration of wear-out failure and random failure;2023 25th European Conference on Power Electronics and Applications (EPE'23 ECCE Europe);2023-09-04
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5. Power Distribution and Propulsion System for an All-Electric Regional Aircraft;2023 IEEE International Conference on Electrical Systems for Aircraft, Railway, Ship Propulsion and Road Vehicles & International Transportation Electrification Conference (ESARS-ITEC);2023-03-29
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