A linear thruster aircraft includes, an aircraft body; an air craft control unit with a processor, a non-transitory memory, and an input/output component; and at least one linear thruster arrangement with at least four thrusters mounted along at least one elongated axis of the aircraft body, such that the thrusters are configured to provide lift, pitch, roll, and yaw movement. Optionally, the linear thruster arrangement can include an alternating lateral offset of the thrusters from the elongated axis.
Aircraft with linear thruster arrangement
2018-12-13
Patent
Elektronische Ressource
Englisch