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Avionics/crew station integrationThe U.S. Navy has been encouraging advanced development concepts aimed at increasing the aircraft instrumentation performance for multi-platform applications of 1990's weapons systems. The three areas covered by the Navy's research and development effort are: System Integration, Technology, and Human Factors. The System Integration objectives are to produce a system architecture easily adaptable to many platforms. Technology objectives are to determine the state of the art for displays, electronics, and controls. The Human Factors objectives are to determine the proper human-machine interfaces so that the ultimate crew station will be capable of providing the pilot with the proper display and controls performance to satisfy the diverse requirements of a fighter, attack, ASW, fixed-wing, rotary-wing, and V/STOL platforms in both a one-man crew or two-man crew matrix. All data/control interface among units of this crew station and other platform subsystems will be via digital data buses and video multiplex buses. No individual discrete signal, data, or control lines will be needed. This paper discusses the six interfaces necessary to ensure the optimum development of this crew station, the predicted platform mission improvements, and the requisite life-cycle cost considerations. This concept will serve as a basis for planning the integration of the necessary hardware and software features in current and future weapons systems.
Document ID
19850006509
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
W. G. Mulley
(Naval Air Development Center Warminster, PA, United States)
Date Acquired
August 12, 2013
Publication Date
December 1, 1984
Publication Information
Publication: Technical Workshop: Advanced Helicopter Cockpit Design Concepts
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Instrumentation
Report/Patent Number
NAS 1.55:2351
REPT-85057
NASA-CP-2351
Meeting Information
Meeting: Technical Workshop: Advanced Helicopter Cockpit Design Concepts
Location: Moffett Field, CA
Country: US
Start Date: July 25, 1983
End Date: July 27, 1983
Sponsors: Ames Helicopter/VTOL Human Factors Office, Aircraft Guidance and Navigation Branch
Accession Number
85N14818
Funding Number(s)
PROJECT: RTOP 536-06-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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