NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Reference energy-altitude descent guidance: Simulator evaluationDescent guidance was developed to provide a pilot with information to ake a fuel-conservative descent and cross a designated geographical waypoint at a preselected altitude and airspeed. The guidance was designed to reduce fuel usage during the descent and reduce the mental work load associated with planning a fuel-conservative descent. A piloted simulation was conducted to evaluate the operational use of this guidance concept. The results of the simulation tests show that the use of the guidance reduced fuel consumption and mental work load during the descent. Use of the guidance also decreased the airspeed error, but had no effect on the altitude error when the designated waypoint was crossed. Physical work load increased with the use of the guidance, but remained well within acceptable levels. The pilots found the guidance easy to use as presented and reported that it would be useful in an operational environment.
Document ID
19850008559
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Abbot, K. H.
(NASA Langley Research Center Hampton, VA, United States)
Knox, C. E.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Instrumentation
Report/Patent Number
NAS 1.60:2383
NASA-TP-2383
L-15800
Report Number: NAS 1.60:2383
Report Number: NASA-TP-2383
Report Number: L-15800
Accession Number
85N16868
Funding Number(s)
PROJECT: RTOP 505-45-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available