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RELIABILITY AND SAFETY ENHANCED ELECTRICAL ACTUATION SYSTEM ARCHITECTURES (RESEARCH)
Start date: Oct 1, 2013, End date: Aug 31, 2016,
The main objective of RESEARCH project is the definition of an electrical architecture for Flight Control System capable of controlling a flight control surface on an Aircraft with the help of electrically operated actuators, thus replacing the hydraulic actuators commonly used in current Aircraft designs.This architecture will be designed with the main objective of being electrical, as this is th ...
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