This document provides a description of a process for development of fly-by-wire actuation systems. Included are (1) the development of requirements for the servo-actuator hardware and the electronics hardware and software, (2) actuator and servo-electronics interface definitions and, (3) the required communications and interactions between the servo-actuator and the servo-electronics designers. ARP5007A has been reaffirmed to comply with the SAE five-year review policy.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Development Process - Aerospace Fly-By-Wire Actuation System


    Publication date :

    2020-10-09



    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Aerospace vehicle actuation systems studies

    Lukase, T. A. / Schissell, G. Z. / Smith, R. M. | NTRS | 1964




    Aerospace Fly-by-Light Actuation Systems

    SAE Technical Papers | 2014