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On Global Optimal Sailplane Flight StrategyThe derivation and interpretation of the necessary conditions that a sailplane cross-country flight has to satisfy to achieve the maximum global flight speed is considered. Simple rules are obtained for two specific meteorological models. The first one uses concentrated lifts of various strengths and unequal distance. The second one takes into account finite, nonuniform space amplitudes for the lifts and allows, therefore, for dolphin style flight. In both models, altitude constraints consisting of upper and lower limits are shown to be essential to model realistic problems. Numerical examples illustrate the difference with existing techniques based on local optimality conditions.
Document ID
19790018902
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sander, G. J.
(Liege Univ.)
Litt, F. X.
(Liege Univ.)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Publication Information
Publication: NASA. Langley Res. Center Sci. and Technol. of Low Speed and Motorless Flight
Subject Category
Aircraft Communications And Navigation
Accession Number
79N27073
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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