Development of an inductor incorporated onto a carbon fiber MAV structural component
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DOI: 10.1007/s00542-016-2958-4
Abstract: Insect-sized flapping wing micro air vehicles (MAVs) are beginning to take flight but have many technical hurdles to overcome. One of the greatest challenges of MAV design is attaining lightweight microelectronic components of optimal size… read more here.
Keywords: onto carbon; carbon fiber; inductor; fiber mav ... See more keywords