Aircraft control method
    1.
    发明授权

    公开(公告)号:US11474540B2

    公开(公告)日:2022-10-18

    申请号:US16907617

    申请日:2020-06-22

    Abstract: A method of automatically determining a flight trajectory of a vertical take-off and landing aircraft having vectorable propulsion can be used to improve flight efficiency. The method includes receiving one or more aircraft flight constraints, inputting the aircraft flight constraints to a trajectory planning algorithm to determine a minimum energy aircraft transition trajectory, and outputting a control schedule to fly the aircraft to along the flight trajectory.

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