• DocumentCode
    2412573
  • Title

    Fly-by-light flight control system development for transport aircraft

  • Author

    Todd, John R.

  • Author_Institution
    McDonnel Douglas Aerosp., Long Beach, CA, USA
  • fYear
    1996
  • fDate
    27-31 Oct 1996
  • Firstpage
    153
  • Lastpage
    158
  • Abstract
    The Fly-By-Light Advanced System Hardware (FLASH) program is developing and demonstrating dual use fly-by-light (FBL) hardware for flight control systems On military and commercial aircraft. Under the transport aircraft portion of this program, we and our industry team-mates are demonstrating two representative fly-by-light systems. These fly-by-light demonstrations include a ground demonstration of a partial primary flight control system and a flight demonstration of-an aileron trim control system. This paper describes these and discusses the dual use fly-by-light hardware developed for transport aircraft as well as the associated FLASH program demonstrations
  • Keywords
    aircraft control; avionics; optical cables; optical fibres; FLASH program demonstration; aileron trim control; closed loop system; commercial aircraft; dual use; fibre optics; fly-by-light flight control; ground demonstration; military aircraft; optical data bus; partial primary flight control; transport aircraft; vehicle management system; Aerospace control; Aerospace electronics; Aerospace industry; Computer architecture; Costs; Defense industry; Electrical equipment industry; Hardware; Military aircraft; Voice mail;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Digital Avionics Systems Conference, 1996., 15th AIAA/IEEE
  • Conference_Location
    Atlanta, GA
  • Print_ISBN
    0-7803-3385-3
  • Type

    conf

  • DOI
    10.1109/DASC.1996.559149
  • Filename
    559149