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Stereo-Video Data Reduction of Wake Vortices and Trailing AircraftsThis report presents stereo image theory and the corresponding image processing software developed to analyze stereo imaging data acquired for the wake-vortex hazard flight experiment conducted at NASA Langley Research Center. In this experiment, a leading Lockheed C-130 was equipped with wing-tip smokers to visualize its wing vortices, while a trailing Boeing 737 flew into the wake vortices of the leading airplane. A Rockwell OV-10A airplane, fitted with video cameras under its wings, flew at 400 to 1000 feet above and parallel to the wakes, and photographed the wake interception process for the purpose of determining the three-dimensional location of the trailing aircraft relative to the wake. The report establishes the image-processing tools developed to analyze the video flight-test data, identifies sources of potential inaccuracies, and assesses the quality of the resultant set of stereo data reduction.
Document ID
19980234597
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Alter-Gartenberg, Rachel
(Computer Sciences Corp. Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1998
Subject Category
Computer Programming And Software
Report/Patent Number
NAS 1.26:208719
NASA/CR-1998-208719
Report Number: NAS 1.26:208719
Report Number: NASA/CR-1998-208719
Funding Number(s)
CONTRACT_GRANT: NAS1-20431
PROJECT: RTOP 548-10-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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