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Optimal aircraft performance during microburst encounterThe effects of microburst characteristics on the optimal penetration performance of jet transport and general aviation aircraft are presented. The purpose is to determine the best possible performance that can be achieved in a broad range of microbursts. A secondary goal is to illustrate good strategies for dealing with a range of microbursts during takeoff and landing. Over 1100 optimal trajectories were computed for two aircraft types flying through idealized microbursts using a Successive Quadratic Programs trajectory optimization algorithm. Contours of safety metrics are plotted as functions of the length scales, magnitudes, and locations of horizontal wind shears and vertical downdrafts. These performance contours show three length-scale regimes for optimal microburst penetration. At short length scales, hazards usually associated with gustiness predominate (e.g., high normal load factor, rotational upset). At intermediate length scales, a degraded ability to maintain flight path and/or vertical velocity poses the most serious threat. At very long microburst length scales, excessive touchdown velocities may result. The ability to transit a microburst successfully also varies strongly with microburst location. The results show that both aircraft types could penetrate some very severe microbursts if optimal control histories were followed. Nevertheless, these control strategies assume perfect prior knowledge of the wind, and practical limits to successful encounter with real-time control capabilities would be lower. The optimally controlled jet transport can successfully penetrate higher intensity microbursts than can the general aviation aircraft.
Document ID
19920008757
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Psiaki, Mark L.
(Cornell Univ. Ithaca, NY., United States)
Stengel, Robert F.
(Princeton Univ. NJ., United States)
Date Acquired
September 6, 2013
Publication Date
December 1, 1991
Publication Information
Publication: NASA. Langley Research Center, Joint University Program for Air Transportation Research, 1990-1991
Subject Category
Air Transportation And Safety
Accession Number
92N17999
Funding Number(s)
CONTRACT_GRANT: NGL-31-001-252
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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