Paper
30 September 1994 Optical fiber sensor arrays to detect impact and damage assessment on board spacecraft and manned platforms
Marc R. H. Voet, Alain R. F. Barel, L. M. Boschmans
Author Affiliations +
Abstract
The rapid growth and implementation of fiber optic sensor devices have evolved to the stage of demonstration and in-situ applications, whereas normally pressure and temperature parameters are measured. New photonic space opto- electronic systems could sense in a distributed way impact, damage assessment and pressure variations in structural integrity testing of spacecraft and platforms. The system consists of several loops (up to 8 per control unit) of fiber optic sensors or cables buried or implemented in smart structures or complex materials in wings or structures. Signal processing has been performed by FDM/TDM techniques to interrogate and to demultiplex unambiguously the fiber optic sensors. The control units could be placed locally or centrally in a network configuration to interrogate up to 256 loops or single sensors.
© (1994) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Marc R. H. Voet, Alain R. F. Barel, and L. M. Boschmans "Optical fiber sensor arrays to detect impact and damage assessment on board spacecraft and manned platforms", Proc. SPIE 2210, Space Optics 1994: Space Instrumentation and Spacecraft Optics, (30 September 1994); https://doi.org/10.1117/12.188073
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KEYWORDS
Sensors

Fiber optics sensors

Composites

Optical fibers

Signal processing

Control systems

Space operations

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