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Simulation and flight studies of an approach profile indicator for VTOL aircraftSimulation and flight investigations were conducted by using a method of providing supplementary information to the pilot in conjunction with a closed-circuit-television display during a VTOL instrument final approach including deceleration and hover. The supplementary information included range, cross range, ground speed, altitude, and rate-of-climb error and was displayed on an instrument called an approach profile indicator. The display was arranged to provide both quasi-command and situation information. Pilot comments indicated that the approach-profile-indicator display concept in conjunction with the closed-circuit television resulted in a decreased pilot workload and an increase in pilot confidence. Also, the results indicated that the approach profile repeatability was significantly improved because of the ground-speed and altitude information provided on the approach profile indicator.
Document ID
19760004969
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Moen, G. C.
(Army Air Mobility R/D Lab. Hampton, Va., United States)
Yenni, K. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1975
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TN-D-8051
L-10204
Report Number: NASA-TN-D-8051
Report Number: L-10204
Accession Number
76N12057
Funding Number(s)
PROJECT: RTOP 505-10-23-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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