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Computer programs for generation and evaluation of near-optimum vertical flight profilesTwo extensive computer programs were developed. The first, called OPTIM, generates a reference near-optimum vertical profile, and it contains control options so that the effects of various flight constraints on cost performance can be examined. The second, called TRAGEN, is used to simulate an aircraft flying along an optimum or any other vertical reference profile. TRAGEN is used to verify OPTIM's output, examine the effects of uncertainty in the values of parameters (such as prevailing wind) which govern the optimum profile, or compare the cost performance of profiles generated by different techniques. A general description of these programs, the efforts to add special features to them, and sample results of their usage are presented.
Document ID
19830016229
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sorensen, J. A.
(Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Waters, M. H.
(Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Patmore, L. C.
(Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Date Acquired
September 4, 2013
Publication Date
May 1, 1983
Publication Information
Publisher: NASA
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AMA-82-39
NASA-CR-3688
NAS 1.26:3688
Report Number: AMA-82-39
Report Number: NASA-CR-3688
Report Number: NAS 1.26:3688
Accession Number
83N24500
Funding Number(s)
CONTRACT_GRANT: NAS1-15497
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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