Results of a Feasibility Study of a Prognostic System for Electro-Hydraulic Flight Control Actuators
Electro-Hydraulic Servo-Actuators (EHSA) are currently the most used actuation technology for primary flight control systems of civil and military aircrafts. Although some alternatives have emerged in the last decade, such as electromechanical or electro-hydrostatic solutions, electrohydraulic syste...
Main Authors: | Sylvain Autin, Andrea De Martin Giovanni Jacazio, Jérôme Socheleau, George Vachtsevanos |
---|---|
Format: | Article |
Language: | English |
Published: |
The Prognostics and Health Management Society
2021-03-01
|
Series: | International Journal of Prognostics and Health Management |
Subjects: | |
Online Access: | https://papers.phmsociety.org/index.php/ijphm/article/view/2935 |
Similar Items
-
A Case Study on the Detection and Prognosis of Internal Leakages in Electro-Hydraulic Flight Control Actuators
by: Antonio Carlo Bertolino, et al.
Published: (2021-08-01) -
Digital hydraulic actuator for flight control
by: Larsson, Felix, et al.
Published: (2019) -
Development and Control of an Electro-Hydraulic Actuator System for an Exoskeleton Robot
by: Dongyoung Lee, et al.
Published: (2019-10-01) -
Design and Performance Evaluation of an Electro-Hydraulic Camless Engine Valve Actuator for Future Vehicle Applications
by: Kanghyun Nam, et al.
Published: (2017-12-01) -
Nonlinearities in Control Description and Design of an Electro Hydraulic Actuator for Flexible Nozzle Thrust Vector Control
by: Dragan Nauparac, et al.
Published: (2018-04-01)