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AssigneeArcher Aviation Inc.
InventorsGeoffrey C. Bower, Nansi Xue, Alan Chen, Benjamin Goldman, Nathan Depenbusch
Estimating the term…
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.
A method of controlling an electric aircraft that comprises a plurality of actuators that includes a plurality of electric propulsion units and a plurality of battery packs that power the plurality of electric propulsion units, the method comprising:
A system for controlling an electric aircraft that comprises a plurality of actuators that includes a plurality of electric propulsion units, the system comprising one or more processors, memory, and one or more programs stored in the memory for execution by the one or more processors for:
Dependencies are inferred from the claim text.