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Characterizing the wake vortex signature for an active line of sight remote sensorA recurring phenomenon, described as a wake vortex, develops as an aircraft approaches the runway to land. As the aircraft moves along the runway, each of the wing tips generates a spiraling and expanding cone of air. During the lifetime of this turbulent event, conditions exist over the runway which can be hazardous to following aircraft, particularly when a small aircraft is following a large aircraft. Left to themselves, these twin vortex patterns will converge toward each other near the center of the runway, harmlessly dissipating through interaction with each other or by contact with the ground. Unfortunately, the time necessary to disperse the vortex is often not predictable, and at busy airports can severely impact terminal area productivity. Rudimentary methods of avoidance are in place. Generally, time delays between landing aircraft are based on what is required to protect a small aircraft. Existing ambient wind conditions can complicate the situation. Reliable detection and tracking of a wake vortex hazard is a major technical problem which can significantly impact runway productivity. Landing minimums could be determined on the basis of the actual hazard rather than imposed on the basis of a worst case scenario. This work focuses on using a windfield description of a wake vortex to generate line-of-sight Doppler velocity truth data appropriate to an arbitrarily located active sensor such as a high resolution radar or lidar. The goal is to isolate a range Doppler signature of the vortex phenomenon that can be used to improve detection. Results are presented based on use of a simplified model of a wake vortex pattern. However, it is important to note that the method of analysis can easily be applied to any vortex model used to generate a windfield snapshot. Results involving several scan strategies are shown for a point sensor with a range resolution of 1 to 4 meters. Vortex signatures presented appear to offer potential for detection and tracking.
Document ID
19950017971
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Heil, Robert Milton
(Clemson Univ. SC, United States)
Date Acquired
September 6, 2013
Publication Date
August 5, 1994
Subject Category
Air Transportation And Safety
Report/Patent Number
NASA-CR-197697
NAS 1.26:197697
TR-080594-4871F
Report Number: NASA-CR-197697
Report Number: NAS 1.26:197697
Report Number: TR-080594-4871F
Accession Number
95N24391
Funding Number(s)
CONTRACT_GRANT: NGT-50975
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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