Adaptive real-time clustering method for dynamic visual tracking of very flexible wings

Journal Article (2021)
Author(s)

T. Mkhoyan (TU Delft - Arts & Crafts, TU Delft - Aerospace Structures & Computational Mechanics)

Coen de de Visser (TU Delft - Control & Simulation)

Roeland Breuker (TU Delft - Aerospace Structures & Computational Mechanics)

Research Group
Aerospace Structures & Computational Mechanics
Copyright
© 2021 T. Mkhoyan, C.C. de Visser, R. De Breuker
DOI related publication
https://doi.org/10.2514/1.I010860
More Info
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Publication Year
2021
Language
English
Copyright
© 2021 T. Mkhoyan, C.C. de Visser, R. De Breuker
Related content
Research Group
Aerospace Structures & Computational Mechanics
Issue number
2
Volume number
18
Pages (from-to)
58-79
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Abstract

Advancements in aircraft controller design, paired with increasingly flexible aircraft concepts, create the need for the development of novel (smart) adaptive sensing methods suitable for aeroelastic state estimation. A potentially universal and noninvasive approach is visual tracking. However, many tracking methods require manual selection of initial marker locations at the start of a tracking sequence. This study aims to address the gap by investigating a robust machine learning approach for unsupervised automatic labeling of visual markers. The method uses fast DBSCAN and adaptive image segmentation pipeline with hue-saturation-value color filter to extract and label the marker centers under the presence of marker failure. In a comparative study, the DBSCAN clustering performance is assessed against an alternative clustering method, the disjoint-set data structure. The segmentation-clustering pipeline with DBSCAN is capable of running real-time at 250 FPS on a single camera image sequence with a resolution of 1088×600 pixels. To increase robustness against noise, a novel formulation (the inverse DBSCAN, DBSCAN−1 ) is introduced. This approach is validated on an experimental dataset collected from camera observations of a flexible wing undergoing gust excitations in a wind tunnel, demonstrating an excellent match with the ground truth obtained with a laser vibrometer measurement system.

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