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Performance limits for optimal microburst encounterAn effort has been made to ascertain the envelope-edges for uneventful aircraft penetrations of microburst windshears on the basis of optimal aircraft control strategies. Over 1100 such trajectories have been computed for contemporary airliners and general aviation aircraft, in the case of idealized microbursts, using a successive quadratic program trajectory optimization algorithm able to directly handle inequality constraints. Variations of optimal performance with microburst type, intensity, length scale, and location, define performance limits; these limits fall into short, intermediate, and long microburst length scale regimes. The ability to safely transit a microburst also varies strongly with microburst location.
Document ID
19880063382
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Psiaki, Mark L.
(Cornell University Ithaca, NY, United States)
Stengel, Robert F.
(Princeton University NJ, United States)
Date Acquired
August 13, 2013
Publication Date
January 1, 1988
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
AIAA PAPER 88-4367
Report Number: AIAA PAPER 88-4367
Meeting Information
Meeting: AIAA Atmospheric Flight Mechanics Conference
Location: Minneapolis, MN
Country: United States
Start Date: August 15, 1988
End Date: August 17, 1988
Accession Number
88A50609
Funding Number(s)
CONTRACT_GRANT: NGL-31-001-252
Distribution Limits
Public
Copyright
Other

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