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User's manual for a fuel-conservative descent planning algorithm implemented on a small programmable calculatorA simplified flight management descent algorithm was developed and programmed on a small programmable calculator. It was designed to aid the pilot in planning and executing a fuel conservative descent to arrive at a metering fix at a time designated by the air traffic control system. The algorithm may also be used for planning fuel conservative descents when time is not a consideration. The descent path was calculated for a constant Mach/airspeed schedule from linear approximations of airplane performance with considerations given for gross weight, wind, and nonstandard temperature effects. An explanation and examples of how the algorithm is used, as well as a detailed flow chart and listing of the algorithm are contained.
Document ID
19840021802
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Vicroy, D. D.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1984
Subject Category
Aircraft Instrumentation
Report/Patent Number
NASA-TM-86275
NAS 1.15:86275
Report Number: NASA-TM-86275
Report Number: NAS 1.15:86275
Accession Number
84N29871
Funding Number(s)
PROJECT: RTOP 505-45-33
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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