SYSTEM AND METHOD FOR UNWANTED FORCE REJECTION AND VEHICLE STABILITY
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United States of America Patent
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Issued Date -
Jul 14, 2016
app pub date -
Sep 25, 2015
filing date -
Sep 25, 2014
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Abstract
An aircraft comprising a fuselage and a plurality of wings. The fuselage may be positioned between a first wing and a second wing, wherein said first wing and said second wing each comprise (a) a plurality of sensors and (b) a plurality of flaperons. A flight controller may be configured to (1) receive measurement data from each of said plurality of sensors and, (2) independently actuate each of said plurality of flaperons.
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