Method for correcting control surface angle measurements in...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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C244S047000

Reexamination Certificate

active

07130725

ABSTRACT:
A 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 from 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 re-computing 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.

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A.W.Burner and Tianshu Liu, “Videogrammetric Model Deformation Measurement Technique,” J. of Aircr., vol. 38 ( No. 4), Jul./Aug. 2001, p. 1-31.

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