Technology Transfer - Technology: Mathematical and Computer Science
Mechanical Engineering - Center of Gravity Determination Apparatus for Fixed Wing Aerial Systems
SSC Atlantic – Patent US, 9,026,350
The general purpose of this invention is to measure the center-of-gravity (CoG) of a micro unmanned aerial system (UAS) to ensure the airframe is properly balanced around the intrinsic CoG. Integrating custom payloads onto the airframe can alter the CoG from the manufactured control position. Therefore, this tool can accurately and precisely measure the airframe’s CoG after payload integration and before flight which allows the user to correct for any CoG differentials.
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