System, a method and a computer program product for maneuvering of an air vehicle with tiltable propulsion unit
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United States of America Patent
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Aug 15, 2017
Grant Date -
Nov 20, 2014
app pub date -
Jan 10, 2013
filing date -
Jan 12, 2012
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Abstract
A control system configured to control a deceleration process of an air vehicle which comprises at least one tiltable propulsion unit, each of the at least one tiltable propulsion units is tiltable to provide a thrust whose direction is variable at least between a general vertical thrust vector direction and a general longitudinal thrust vector direction with respect to the air vehicle.
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