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Method for Correcting Control Surface Angle Measurements in Single Viewpoint PhotogrammetryA method of determining a corrected control surface angle for use in single viewpoint photogrammetry to correct control surface angle measurements affected by wing bending. First and second visual targets are spaced apart &om one another on a control surface of an aircraft wing. The targets are positioned at a semispan distance along the aircraft wing. A reference target separation distance is determined using single viewpoint photogrammetry for a "wind off condition. An apparent target separation distance is then computed for "wind on." The difference between the reference and apparent target separation distances is minimized by recomputing the single viewpoint photogrammetric solution for incrementally changed values of target semispan distances. A final single viewpoint photogrammetric solution is then generated that uses the corrected semispan distance that produced the minimized difference between the reference and apparent target separation distances. The final single viewpoint photogrammetric solution set is used to determine the corrected control surface angle.
Document ID
20070003564
Acquisition Source
Headquarters
Document Type
Other - Patent
Authors
Burner, Alpheus W.
Barrows, Danny A.
Date Acquired
August 24, 2013
Publication Date
October 31, 2006
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
Patent Number: US-Patent-7,130725
Patent Number: NASA-Case-LAR-17021-1
Patent Application Number: US-Patent-Appl-SN-239457
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
US-Patent-7,130725|NASA-Case-LAR-17021-1
Patent Application
US-Patent-Appl-SN-239457
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