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Concepts for generating optimum vertical flight profilesAlgorithms for generating optimum vertical profiles are derived and examined. These algorithms form the basis for the design of onboard flight management concepts. The variations in the optimum vertical profiles (resulting from these concepts) due to variations in wind, takeoff weight, and range-to-destination are presented. Further considerations for mechanizing two different onboard methods of computing near-optimum flight profiles are then outlined. Finally, the results are summarized, and recommendations are made for further work. Technical details of optimum trajectory design, steering requirements for following these trajectories, and off-line computer programs for testing the concepts are included.
Document ID
19800009767
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sorensen, J. A.
(Analytical Mechanics Associates, Inc. Mountain View, CA, United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-CR-159181
Report Number: NASA-CR-159181
Accession Number
80N18031
Funding Number(s)
CONTRACT_GRANT: NAS1-15497
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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