NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Design and evaluation of a cockpit display for hovering flightA simulator evaluation of a cockpit display format for hovering flight is described. The display format is based on the position-velocity-acceleration representation (PVA) similar to that used in the Pilot Night Vision System in the Army AH-64 helicopter. By only varying the nature of the display law driving the primary indicator in the PVA format, i.e., the acceleration symbol, three candidate displays are created and evaluated. These range from a Status display in which the primary indicator provides true acceleration information to a Command display, in which the primary indicator provides flight director information. Simulation results indicate that two of the three displays offer performance and handling qualities which make them excellent candidates for future helicopter cockpit display systems.
Document ID
19890001529
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hess, Ronald A.
(California Univ. Davis, CA, United States)
Gorder, Peter James
(California Univ. Davis, CA, United States)
Date Acquired
September 5, 2013
Publication Date
October 2, 1988
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-183247
NAS 1.26:183247
Accession Number
89N10900
Funding Number(s)
CONTRACT_GRANT: NCC2-383
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available