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.
System, a method and a computer program product for maneuvering of an air vehicle with tiltable propulsion unit
2019-11-12
Patent
Elektronische Ressource
Englisch
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