Paper
12 July 1993 Simultaneous single-fiber active vibration sensing and impact detection for large space structures
Peter L. Fuhr
Author Affiliations +
Abstract
The increasing complexity of large space structures further emphasizes the need for multi-use single element spacecraft components and sensors. Sensing of the vibrations of components and/or sections of a large space structure is necessary for ultra-high precision pointing and tracking as well as general platform stability. At the same time, the quest for a method of detecting spacecraft impacts with micrometeorites or debris continues. In this paper a method for using a single optical fiber for simultaneous impact detection and vibration sensing is described. Laboratory studies of these techniques using composite material panels are presented.
© (1993) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Peter L. Fuhr "Simultaneous single-fiber active vibration sensing and impact detection for large space structures", Proc. SPIE 1918, Smart Structures and Materials 1993: Smart Sensing, Processing, and Instrumentation, (12 July 1993); https://doi.org/10.1117/12.147971
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CITATIONS
Cited by 4 scholarly publications.
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KEYWORDS
Fiber optics sensors

Sensors

Modulation

Optical fibers

Composites

Active remote sensing

Space operations

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