NASA NTRS · 20030000845
Uncertainty of Videogrammetric Techniques used for Aerodynamic Testing
Abstract
The uncertainty of videogrammetric techniques used for the measurement of static aeroelastic wind tunnel model deformation and wind tunnel model pitch angle is discussed. Sensitivity analyses and geometrical considerations of uncertainty are augmented by analyses of experimental data in which videogrammetric angle measurements were taken simultaneously with precision servo accelerometers corrected for dynamics. An analysis of variance (ANOVA) to examine error dependence on angle of attack, sensor used (inertial or optical). and on tunnel state variables such as Mach number is presented. Experimental comparisons with a high-accuracy indexing table are presented. Small roll angles are found to introduce a zero-shift in the measured angles. It is shown experimentally that. provided the proper constraints necessary for a solution are met, a single- camera solution can he comparable to a 2-camera intersection result. The relative immunity of optical techniques to dynamics is illustrated.
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Burner, A. W., Liu, Tianshu, DeLoach, Richard. 2002-01-01. Uncertainty of Videogrammetric Techniques used for Aerodynamic Testing. https://ntrs.nasa.gov/citations/20030000845
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