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
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