Zobrazeno 1 - 9
of 9
pro vyhledávání: '"Benedetto Luciano"'
Publikováno v:
Aerospace, Vol 9, Iss 9, p 527 (2022)
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 applicati
Externí odkaz:
https://doaj.org/article/648b067ad552455f9149d3bc36453873
Publikováno v:
Actuators, Vol 10, Iss 9, p 230 (2021)
The work deals with the development of deterministic model-based condition-monitoring algorithms for an electromechanical flight control actuator with fault-tolerant architecture, in which two permanent magnets synchronous motors are coupled with dif
Externí odkaz:
https://doaj.org/article/3bd4acd0bb4049348f1371aa268f8799
Publikováno v:
Sensors, Vol 20, Iss 4, p 950 (2020)
The paper deals with theoretical and experimental studies for the development of a self-powered structural health monitoring (SHM) system using macro-fiber composite (MFC) patches. The basic idea is to integrate the actuation, sensing, and energy har
Externí odkaz:
https://doaj.org/article/5870ecc539f14e9990c9276b604f674c
Autor:
Mario R. Chiarelli, Gianpietro Di Rito, Benedetto Luciano, Ivan J. Miralles Irles, Enrico Liberatori, Luca Bancallari
Publikováno v:
2022 IEEE 9th International Workshop on Metrology for AeroSpace (MetroAeroSpace).
Publikováno v:
2021 IEEE 8th International Workshop on Metrology for AeroSpace (MetroAeroSpace).
The paper deals with the development and the performance characterisation of a sensor-fusion technique aiming to the reconstruction of the motor speed feedback in a compact EMA for primary flight control applications. The technique is based on the co
Publikováno v:
Actuators
Volume 10
Issue 9
Actuators, Vol 10, Iss 230, p 230 (2021)
Volume 10
Issue 9
Actuators, Vol 10, Iss 230, p 230 (2021)
The work deals with the development of deterministic model-based condition-monitoring algorithms for an electromechanical flight control actuator with fault-tolerant architecture, in which two permanent magnets synchronous motors are coupled with dif
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::80dbd39a356dc1bb398dc3a1272a85f7
http://hdl.handle.net/11568/1106552
http://hdl.handle.net/11568/1106552
Publikováno v:
2020 IEEE 7th International Workshop on Metrology for AeroSpace (MetroAeroSpace).
The paper deals with the theoretical and experimental development of model-based health-monitoring algorithms for a jamming-tolerant electromechanical actuator for flight control applications. A nonlinear dynamic model of the actuator, which includes
The paper deals with theoretical and experimental studies for the development of model-based condition-monitoring algorithms of composite laminates equipped with piezoelectric Macro-Fiber Composite patches. Starting from the experimental characterisa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::821c9cddd9bdef26b34338e1d59f1d53
http://hdl.handle.net/11568/992965
http://hdl.handle.net/11568/992965
Publikováno v:
Sensors (Basel, Switzerland)
Sensors
Volume 20
Issue 4
Sensors, Vol 20, Iss 4, p 950 (2020)
Sensors
Volume 20
Issue 4
Sensors, Vol 20, Iss 4, p 950 (2020)
The paper deals with theoretical and experimental studies for the development of a self-powered structural health monitoring (SHM) system using macro-fiber composite (MFC) patches. The basic idea is to integrate the actuation, sensing, and energy har