Advanced Flight Control Actuation Systems and Their Interface with Digital Commands Fairey Hydraulics Limited, Hounslow, England

Format:

Conference/Event

Author/Creator:

Anthony, M. J., author.

Conference Name:

A-6 Symposium Program Advanced Actuation, Controls, and Integration for Aerospace Vehicles (1985-10-07 : San Diego, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1985

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

851754

Access Restriction:

Restricted for use by site license