DocumentCode
2839282
Title
Digital flight control systems: some new commercial twists
Author
Todd, John R. ; Yount, Larry J.
Author_Institution
McDonnell Douglas Corp., Long Beach, CA, USA
fYear
1991
fDate
14-17 Oct 1991
Firstpage
79
Lastpage
84
Abstract
The exponential increase in the number and complexity of aircraft digital electronic systems over the last decade has brought to light a number of fault and failure mechanisms not encountered with traditional mechanical and analog systems. One approach to handling these problems on future commercial aircraft is through the use of integrated modular avionics (IMAs). The issues and concepts associated with commercial IMAs are discussed. Some integration concepts for future fly-by-wire/fly-by-light commercial aircraft are considered. It is likely that highly integrated commercial modular avionics systems will be in service by the late 1990s or early twenty first century. It is expected that the extent and rapidity of modular avionics applications on commercial transport will depend largely on the flexibility and fault tolerance achievable at a reasonable cost as well as on the need for incorporation of new highly integrated systems
Keywords
aircraft control; aircraft instrumentation; digital control; modules; aircraft digital electronic systems; digital flight control systems; failure mechanisms; fault mechanisms; fly-by-light commercial aircraft; fly-by-wire aircraft; integrated modular avionics; Aerospace control; Aerospace electronics; Aircraft propulsion; Certification; Computer architecture; Costs; Failure analysis; Fault tolerance; Glass; Military aircraft;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1991. Proceedings., IEEE/AIAA 10th
Conference_Location
Los Angeles, CA
Type
conf
DOI
10.1109/DASC.1991.177147
Filename
177147
Link To Document