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Figure 2: Close-up of constructed camera system with: (bottom) twoboard-level cameras in pan-tilt unit; (right) GNSS receiver mounted ontop of the UAV during flight; (top) single-board-computer interfacing thecameras and the GNSS receiver.
Figure 5:Raw
Figure 6: x and y pixel velocities under rotation of the camera (max. an-gular velocity) plotted against the pixel distance from the principal point.Results plotted for pinhole camera model (top) and distortion cameramodel (bottom).
Figure 8 shows the result of our calibration measurement seriesfor each of the channels
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