DESIGN AND DEVELOPMENT OF STRUCTURALLY FEASIBLE SMALL UNMANNED AERIAL VEHICLES
This study is focused on designing conformal antennas to be deployed with the inflatable wings for unmanned aerial vehicles (UAV). The main emphasis is on utilizing the structure of the wing to develop antennas for various frequency bands, while maintaining the wing’s aerodynamic performance. An ant...
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| Format: | Others |
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UKnowledge
2010
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| Online Access: | http://uknowledge.uky.edu/gradschool_theses/5 http://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1003&context=gradschool_theses |