DocumentCode
1710748
Title
Integrating fly-by-light systems
Author
Todd, John R. ; Hay, John A. ; Brennan, Michael E.
Author_Institution
McDonnell Douglas Corp., Long Beach, CA, USA
fYear
1992
Firstpage
411
Lastpage
416
Abstract
The authors describe how new systems, technologies, and functions will be integrated into the ACAS (aircraft controls and avionics system) fly-by-light architecture, and discuss some of the current Douglas Aircraft development work associated with it. The ACAS integrated fly-by-light architecture will provide improved performance, operational capabilities, manufacturability and maintainability, upgradability, and cross type adaptability. The success of this highly integrated fly-by-light architecture is tied to multidisciplinary holistic development approach and the large-scale application of modularization. The application of fly-by-light technologies to control and sensing functions could substantially reduce the electromagnetic susceptibility of critical electronic flight control systems while preserving their benefits
Keywords
aerospace computer control; aircraft instrumentation; computerised instrumentation; interference suppression; military systems; optical fibres; optical interconnections; peripheral interfaces; Douglas Aircraft development; aircraft controls; avionics; cross type adaptability; electromagnetic susceptibility; fly-by-light architecture; fly-by-light systems; maintainability; manufacturability; upgradability; Aerospace control; Aerospace electronics; Aircraft propulsion; Bandwidth; Control systems; Electromagnetic interference; Electromagnetic shielding; Military aircraft; Optical fibers; Protection;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1992. Proceedings., IEEE/AIAA 11th
Conference_Location
Seattle, WA
Print_ISBN
0-7803-0820-4
Type
conf
DOI
10.1109/DASC.1992.282124
Filename
282124
Link To Document