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Practical solutions to the aircraft minimum fuel, fixed-range, fixed time-of-arrival trajectory optimization problemA practical scheme is presented for generating fixed range, minimum fuel vertical flight profiles that also satisfy time-of-arrival constraints. The resulting algorithm is suitable for incorporation into an on-board flight management system. Example results show that such a capability can save up to 6% of fuel burned in flights subject to delays because of terminal area congestion.
Document ID
19810061111
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
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)
Date Acquired
August 11, 2013
Publication Date
January 1, 1980
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: Joint Automatic Control Conference
Location: San Francisco, CA
Start Date: August 13, 1980
End Date: August 15, 1980
Accession Number
81A45515
Funding Number(s)
CONTRACT_GRANT: NAS1-15497
Distribution Limits
Public
Copyright
Other

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