Fault‐tolerant drive system based on the redundancy bridge arm for aerospace applications
Author:
Affiliation:
1. School of AutomationNanjing University of Science and TechnologyNanjing210094People's Republic of China
2. College of Automation EngineeringNanjing University of Aeronautics and AstronauticsNanjing211106People's Republic of China
Funder
Fundamental Research Funds for the Central Universities
Publisher
Institution of Engineering and Technology (IET)
Subject
Electrical and Electronic Engineering
Link
https://onlinelibrary.wiley.com/doi/pdf/10.1049/iet-epa.2017.0650
Reference25 articles.
1. Robust Control of Fault-Tolerant Permanent-Magnet Synchronous Motor for Aerospace Application With Guaranteed Fault Switch Process
2. Design of a Five-Phase Brushless DC Motor for a Safety Critical Aerospace Application
3. Analysis of a dual‐winding fault‐tolerant permanent magnet machine drive for aerospace applications;Jiang X.;IEEE Trans. Magn.,2015
4. Overview of Electric Motor Technologies Used for More Electric Aircraft (MEA)
5. Electric drive system of dual‐winding fault‐tolerant permanent magnet motor for aerospace applications;Jiang X.;IEEE Trans. Ind. Electron.,2015
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