Optimal control of electromechanical aerospace actuators for reduction of energy losses
With continuous efforts to optimize performance and reduce operational and maintenance costs, the aircraft industry is rapidly pushing towards the concept of all or more-electric aircraft (MEA). Today’s flight control systems being largely hydraulically powered, are gradually turning into electromec...
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| Format: | Thesis |
| Language: | English |
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2019
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| Online Access: | http://hdl.handle.net/10356/79011 |