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Flight Displays for the Next Generation Aircraft
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English
Abstract
The influence of the increasing complexity of the commercial transport operating environment is cited as the reason for applying advanced display technology to new aircraft design. Principal factors are the fuel crisis, sensitivity of the environmental noise, and the need for increased traffic capacity. Industry-wide development programs for fully configured flight decks, as well as specific subsystems, are reviewed.
Citation
Dunn, R., "Flight Displays for the Next Generation Aircraft," SAE Technical Paper 760930, 1976, https://doi.org/10.4271/760930.Also In
References
- Roscoe, S. N. et al “Advanced Integrated Aircraft Displays and Augmented Flight Control.” Aviation Research Laboratory University of Illinois Champaign-Urbana ARL-75-12/ONR-75-2 June 1975
- Bateman L. F. “An Evolutionary Approach to the Design of Flight Decks for Future Civil Transport Aircraft.” Guild of Air Pilots and Air Navigators September 9 1976
- Parks, D. L. et al “Development of an Independent Altitude Monitor Concept.” Report No. FAA-RD-73-168 September 1973
- Smith, W. D. et al “Independent Altitude Monitor Alert Methods and Modes Study.” Report No. FAA-RD-75-86 July 1975
- Graham, D. K. “A Procedure for the Design of Multifunction Switching Controls.” JANAIR Report 740702 August 1971
- Graham, D. K. et al “Annual Technical Report, Cockpit Switching Study, Phase 3, Technology and Interface Requirements for Multifunction Switching/Display Systems, D180-18732-1.” The Boeing Aerospace Company June 1975