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Vibrometer Steering System for Dynamic In-flight Tracking and Measurement
Authors:A Jennings  J Black  C Allen  J Simpkins  R Sollars
Institution:(1) Southern Ohio Council for Higher Education, 3155 Research Blvd, Suite 204, Dayton, OH 45420, USA;(2) Dept. of Aeronautics and Astronautics, Air Force Institute of Technology, 2905 Hobson Way, WPAFB, OH 45433, USA;(3) Dept. of Engineering Science, Trinity University, 1 Trinity Place, San Antonio, TX 78212-7200, USA;(4) Present address: 275 Fizpatrick Hall, Notre Dame, IN 46556, USA
Abstract:A noncontact measurement system is developed for measuring lightweight flexible structures in motion by steering a vibrometer beam to a point on the structure located by videogrammetry. Triangulation of video data, videogrammetry, can capture large scale motion in near real-time, but has limited data collection rates and spatial resolution. Laser vibrometry can capture minute structural vibrations but requires precise alignment. This paper presents a method to register a vibrometry system within a videogrammetry system so that the vibrometer can be steered to sub-degree accuracy. Because videogrammetry is data intensive, there is some processing delay resulting in tracking error. By using a Kalman filter, dynamic tracking error can be reduced by half. Vibration results compared to baseline cases show no impairment to natural frequency measurement. The dynamic in-flight tracking and measurement system will allow testing of more sensitive structures such as flexible wing air vehicles or deployable space structures.
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