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Electrically Powered Actuation for Civil Aircraft Applications
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| Author(s) |
Richard M Crowder |
| Abstract |
The predicted future changes in the operation of civil aircraft has required aircraft manufacturers and equipment suppliers to develop new system concepts, including power- and
fly-by-wire. One aspect of this work is the development of high performance electrically powered actuators. This paper discuss the operation and simulation of a electrohydrostatic
actuator for power by wire applications. |
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| Filename: | Unnamed file |
| Filesize: | 369 KB |
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| Type |
Members Only |
| Date |
Last modified 2018-04-12 by System |
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