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Optimal flight paths through microburst wind profilesThe problem of safe microburst wind shear encounter during the approach and climb-out flight phases is addressed using flight path optimization. The purpose was to investigate the physical limits of safe penetration and to determine control strategies that take full advantage of those limits. Optimal trajectories for both jet transport and general aviation aircraft were computed for encounters with idealized and actual microburst profiles. The results demonstrate that limits to control system design rather than to the aircraft's physical performance may be the deciding factor in an aircraft's capability for safe passage through a wide class of microbursts. The best control strategies responded to airspeed loss in an unconventional manner: by raising the nose to maintain lift.
Document ID
19850061721
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Psiaki, M. L.
(Princeton Univ. NJ, United States)
Stengel, R. F.
(Princeton University NJ, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1985
Subject Category
Aircraft Stability And Control
Report/Patent Number
AIAA PAPER 85-1833
Meeting Information
Meeting: Atmospheric Flight Mechanics Conference
Location: Snowmass, CO
Start Date: August 19, 1985
End Date: August 21, 1985
Accession Number
85A43872
Funding Number(s)
CONTRACT_GRANT: NGL-31-001-252
Distribution Limits
Public
Copyright
Other

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