Conference
Study of Different Architectures of Fault-Tolerant Actuator Using a Two-Channel PM Motor
Abstract
In the context of more electric aircraft, the use of electric actuators instead of hydraulic ones is one of the main topics of research and development in electrical engineering. A high level of reliability, the redundancy, and the compactness are required for aircraft electrical actuators. For achieving these purposes, a classical solution consists in using two identical actuators motorized by one permanent magnet (PM) motor supplied by a …
Authors
Vaseghi B; Takorabet N; Caron JP; Nahid-Mobarakeh B; Meibody-Tabar F; Humbert G
Volume
47
Pagination
pp. 47-54
Publisher
Institute of Electrical and Electronics Engineers (IEEE)
Publication Date
January 1, 2011
DOI
10.1109/tia.2010.2090930
Conference proceedings
IEEE Transactions on Industry Applications
Issue
1
ISSN
0093-9994