Minimisation of Failure Transients in a Fail-Safe Electro-Mechanical Actuator Employed for the Flap Movables of a High-Speed Helicopter-Plane

Minimisation of Failure Transients in a Fail-Safe Electro-Mechanical Actuator Employed for the Flap Movables of a High-Speed Helicopter-Plane

The work deals with the model-based characterization of the failure transients of a fail-safe rotary EMA developed by Umbragroup (Italy) for the flap movables of the RACER helicopter-plane by Airbus Helicopters (France). Since the reference application requires quasi-static position-tracking with hi...

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Bibliographic Details
Main Authors: Gianpietro Di Rito, Romain Kovel, Marco Nardeschi, Nicola Borgarelli, Benedetto Luciano
Format: Article
Language:English
Published: MDPI AG 2022-09-01
Series:Aerospace
Subjects:
health monitoring
electro-mechanical actuators
modelling
simulation
testing
flight control
Online Access:https://www.mdpi.com/2226-4310/9/9/527

Internet

https://www.mdpi.com/2226-4310/9/9/527

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