NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Estimation of Separation Buffers for Wind-Prediction Error in an Airborne Separation Assistance SystemWind prediction errors are known to affect the performance of automated air traffic management tools that rely on aircraft trajectory predictions. In particular, automated separation assurance tools, planned as part of the NextGen concept of operations, must be designed to account and compensate for the impact of wind prediction errors and other system uncertainties. In this paper we describe a high fidelity batch simulation study designed to estimate the separation distance required to compensate for the effects of wind-prediction errors throughout increasing traffic density on an airborne separation assistance system. These experimental runs are part of the Safety Performance of Airborne Separation experiment suite that examines the safety implications of prediction errors and system uncertainties on airborne separation assurance systems. In this experiment, wind-prediction errors were varied between zero and forty knots while traffic density was increased several times current traffic levels. In order to accurately measure the full unmitigated impact of wind-prediction errors, no uncertainty buffers were added to the separation minima. The goal of the study was to measure the impact of wind-prediction errors in order to estimate the additional separation buffers necessary to preserve separation and to provide a baseline for future analyses. Buffer estimations from this study will be used and verified in upcoming safety evaluation experiments under similar simulation conditions. Results suggest that the strategic airborne separation functions exercised in this experiment can sustain wind prediction errors up to 40kts at current day air traffic density with no additional separation distance buffer and at eight times the current day with no more than a 60% increase in separation distance buffer.
Document ID
20090026008
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Consiglio, Maria C.
(NASA Langley Research Center Hampton, VA, United States)
Hoadley, Sherwood T.
(NASA Langley Research Center Hampton, VA, United States)
Allen, B. Danette
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 24, 2013
Publication Date
June 29, 2009
Subject Category
Air Transportation And Safety
Report/Patent Number
Lf99-8317
Report Number: Lf99-8317
Meeting Information
Meeting: 8th USA-Europe Research and Development Seminar - ATM 2009
Location: Napa, CA
Country: United States
Start Date: June 29, 2009
End Date: July 2, 2009
Funding Number(s)
WBS: WBS 411931.02.51.07.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available