Adaptive Load Control of Flexible Aircraft Wings Using Fiber Optic Sensing

Francisco Pena; Benjamin Martins; W. Lance Richards

doi:10.1364/OFS.2018.WF101

26th International Conference on Optical Fiber Sensors
OSA Technical Digest (Optica Publishing Group, 2018),
paper WF101
•https://doi.org/10.1364/OFS.2018.WF101

Adaptive Load Control of Flexible Aircraft Wings Using Fiber Optic Sensing

Francisco Pena, Benjamin Martins, and W. Lance Richards

Optical Fiber Sensors 2018

Lausanne Switzerland
24–28 September 2018
ISBN: 978-1-943580-50-7

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Poster Session II (WF)

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F. Pena, B. Martins, and W. L. Richards, "Adaptive Load Control of Flexible Aircraft Wings Using Fiber Optic Sensing," in 26th International Conference on Optical Fiber Sensors, OSA Technical Digest (Optica Publishing Group, 2018), paper WF101.

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Abstract

Eighteen-hundred fiber Bragg grating strain sensors characterized the aircraft wing strain-state and displacement in real time during flight. The control system tracked a 1 g tip-displacement profile while actively minimizing the root strain and tip displacement.

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