Development of a high force density, actuation drive for an aerospace application
This paper deals with the design, implementation and experimental validation of a complete, electrical drive system, for linear actuation in an aerospace environment, with the main requirements being high force/power density, reliability, availability and fault tolerance. A directly-driven, linear,...
| Main Authors: | , |
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| Format: | Conference or Workshop Item |
| Language: | English |
| Published: |
2018
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| Subjects: | |
| Online Access: | https://eprints.nottingham.ac.uk/55157/ |