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1.发明公开
公开(公告)号：EP4324745A3
公开(公告)日：2024-05-15
申请号：EP23220866.0
申请日：2022-01-24
CPC分类号： B64C29/0033 , B64C2220/0020130101 , B64C11/46 , B64C11/30 , Y02T50/60 , B64D27/357 , B64D31/16
摘要： A method of controlling an electric aircraft that has a plurality of actuators that includes a plurality of electric propulsion units includes: receiving force and moment commands for the electric aircraft; determining control commands for the plurality of actuators based on the desired force and moment commands by solving an optimization problem that comprises a noise minimization term for minimizing noise generated by the electric propulsion units; and controlling the plurality of actuators according to the determined control commands to meet the force and moment commands for the electric aircraft.
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2.发明公开
公开(公告)号：EP4324745A2
公开(公告)日：2024-02-21
申请号：EP23220866.0
申请日：2022-01-24
IPC分类号： B64D27/24
摘要： A method of controlling an electric aircraft that has a plurality of actuators that includes a plurality of electric propulsion units includes: receiving force and moment commands for the electric aircraft; determining control commands for the plurality of actuators based on the desired force and moment commands by solving an optimization problem that comprises a noise minimization term for minimizing noise generated by the electric propulsion units; and controlling the plurality of actuators according to the determined control commands to meet the force and moment commands for the electric aircraft.
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3.发明公开
公开(公告)号：EP4281365A1
公开(公告)日：2023-11-29
申请号：EP22703539.1
申请日：2022-01-24
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