Drive-system optimisation for a helicopter electromechanical actuation system
More-electric aircraft architectures are an approach to increase the efficiency of aircraft as well as to reduce the environmental impact and operational costs. This thesis describes concepts for electromechanical actuation systems for a helicopter primary flight control application. This work has b...
| Main Author: | |
|---|---|
| Published: |
University of Nottingham
2014
|
| Subjects: | |
| Online Access: | http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.718988 |