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Title: |
State-of-the-art cockpit design for the HH-65A helicopters
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Author(s): |
Castleberry, D. E.; Mcelreath, M. Y.
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Abstract: |
In the design of a HH-65A helicopter cockpit, advanced integrated electronics systems technology was employed to achieve several important goals for this multimission aircraft. They were: (1) integrated systems operation with consistent and simplified cockpit procedures; (2) mission-task-related cockpit displays and controls, and (3) reduced pilot instrument scan effort with excellent outside visibility. The integrated avionics system was implemented to depend heavily upon distributed but complementary processing, multiplex digital bus technology, and multifunction CRT controls and displays. This avionics system was completely flight tested and will soon enter operational service with the Coast Guard.
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NASA Center: |
NASA (non Center Specific)
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Publication Date: |
Apr 1, 1982
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Document Source: |
CASI |
No Digital Version Available: |
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Document ID: |
19820015346
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Accession ID: |
82N23220
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Publication Information: |
NASA. Ames Research Center Helicopter Handling Qualities, p 139-143, Number of Pages = 5 |
Price Code: |
A01 |
Keywords: |
AIRCRAFT CONTROL; AIRCRAFT DESIGN; COCKPITS; DISPLAY DEVICES; FLIGHT CONTROL; MILITARY HELICOPTERS; AIRCRAFT COMPARTMENTS; CATHODE RAY TUBES; COMPUTER TECHNIQUES; CONTROL; DATA PROCESSING; DIGITAL SYSTEMS; FLIGHT TESTS; MILITARY TECHNOLOGY; MULTIPLEXING; VIDEO EQUIPMENT;
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Notes: |
In NASA. Ames Research Center Helicopter Handling Qualities p 139-143 (SEE N82-23208 14-03) |
Accessibility: |
Unclassified; Copyright; Unlimited; Publicly available; |
Updated/Added to NTRS: |
2009-01-14 |
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