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TERMINÉ
REconfiguration of CONtrol in Flight for Integral Global Upset REcovery (RECONFIGURE)
Date du début: 1 janv. 2013, Date de fin: 30 juin 2016,
Commercial aircraft fault tolerant control (FTC) strategies in the flight control system (FCS) are based on fail-safe approaches whereby a nominal control law is switched first to a robust solution and then if necessary to a direct law controlling the actuators surfaces. Each component of the control law set is designed off-line and has a different level of robustness and performance. The reasons ...
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TERMINÉ
ACTUATION 2015: Modular Electro Mechanical Actuators for ACARE 2020 Aircraft and Helicopters (ACTUATION2015)
Date du début: 1 nov. 2011, Date de fin: 30 avr. 2016,
The All-Electric Aircraft is a major target for the next generation of aircraft to lower consumption of non-propulsive power and thus fuel burn. To eliminate hydraulic circuits, pumps and reservoirs, Electro Mechanical Actuators (EMA) are mandatory but now need to meet cost, reliability and weight requirements from the airframers.ACTUATION2015 aims to develop and validate a common set of standard ...
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