It is disclosed a distributed electric propulsion fixed-wing aircraft comprising a plurality of propulsive units, wherein propulsive units are arranged symmetrically with respect to the longitudinal plane, wherein of propulsive units comprises first propulsive units at a first side of the longitudinal plane and second propulsive units at a second side of the longitudinal plane, wherein the distributed propulsion aircraft further comprises a control unit configured to provide a yawing moment so that a sideslip angle is generated, so that the distributed electric propulsion aircraft flies as a fixed-wing aircraft equipped with a single propeller.

Distributed Electric Propulsion Aircraft Simulating a Single Propeller Aircraft

Trainelli, L.;Riboldi, C. E. D.;
2021-01-01

Abstract

It is disclosed a distributed electric propulsion fixed-wing aircraft comprising a plurality of propulsive units, wherein propulsive units are arranged symmetrically with respect to the longitudinal plane, wherein of propulsive units comprises first propulsive units at a first side of the longitudinal plane and second propulsive units at a second side of the longitudinal plane, wherein the distributed propulsion aircraft further comprises a control unit configured to provide a yawing moment so that a sideslip angle is generated, so that the distributed electric propulsion aircraft flies as a fixed-wing aircraft equipped with a single propeller.
2021
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11311/1176827
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