Advanced Flight Control Actuation Systems and Their Interface with Digital Commands 851754
Advanced flight control actuation systems require that the actuator be capable of interfacing with centralised digital computing systems.
The actuation specialist must consider the electro hydraulic system as a whole, including the closed loop servo electronics, from the command distribution databus to the final output member.
This paper discusses the overall approach of a primary flight control specialist company, with the lateral implications of direct drive and multi redundant valve configurations, higher system pressures and direct rotary actuation.
Citation: Anthony, M. and Mattos, F., "Advanced Flight Control Actuation Systems and Their Interface with Digital Commands," SAE Technical Paper 851754, 1985, https://doi.org/10.4271/851754. Download Citation
Author(s):
M. J. Anthony, F. Mattos
Affiliated:
Fairey Hydraulics Ltd., Hounslow, England
Pages: 16
Event:
A-6 Symposium Program Advanced Actuation, Controls, and Integration for Aerospace Vehicles
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Hydraulic systems
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