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A study of altitude and flight path angle dynamics for a singularly perturbed fuel optimization problemThis short paper will demonstrate that the separation of altitude and flight path angle dynamics using singular perturbation techniques for a transport fuel optimization problem results in an unacceptable oscillation in altitude. A technique for damping this oscillation by adding a penalty term to the cost function for the optimization problem will be discussed. This technique will be compared with a different approach that linearizes the altitude and flight path angle boundary layers.
Document ID
19840042720
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Price, D. B.
(NASA Langley Research Center Hampton, VA, United States)
Gracey, C.
(NASA Langley Research Center Flight Dynamics and Control Div., Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1983
Subject Category
Aircraft Design, Testing And Performance
Accession Number
84A25507
Distribution Limits
Public
Copyright
Other

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