Orbital Debris Conference: Technical Issues andFuture Directions 1990
DOI: 10.2514/6.1990-1275
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Advanced parameter identification techniques for near real time flight flutter test analysis

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Cited by 6 publications
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“…On the top right we see the global power spectrum recovered from the video. On the bottom left we see the modal image for a predicted flex mode at 2.5245 Hz, which is less than 3% off from the reported value of 2.584 Hz [20]. The modal image is for the x dimension of the video.…”
Section: Modal Imaging In the Wildmentioning
confidence: 95%
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“…On the top right we see the global power spectrum recovered from the video. On the bottom left we see the modal image for a predicted flex mode at 2.5245 Hz, which is less than 3% off from the reported value of 2.584 Hz [20]. The modal image is for the x dimension of the video.…”
Section: Modal Imaging In the Wildmentioning
confidence: 95%
“…He was then able to find a reference for the dominant flex mode of that aircraft, which was reported as 2.584 Hz [20]. This is less than 3% off from the frequency we predicted from video.…”
Section: Modal Imaging In the Wildmentioning
confidence: 99%