Patent ID: 11952105
Assignee: BETA TECHNOLOGIES, INC.
Field: Control (Instruments)
Classification: CPC B  G  H | IPC B  H

Claim 0:
1. A system for flight control in electric aircraft, the system comprising:
a flight controller, wherein the flight controller is configured to provide an initial vehicle torque signal comprising a plurality of attitude commands;
a mixer, wherein the mixer includes circuitry configured to:
receive the initial vehicle torque signal;
receive at least a vehicle torque limit;
receive a plurality of prioritization data, the plurality of prioritization data including a prioritization datum corresponding to each of the plurality of attitude commands;
determine a plurality of modified attitude commands as a function of the at least a vehicle torque limit, the plurality of attitude commands, and the plurality of prioritization data;
generate, as a function of the plurality of modified attitude commands, an output torque command, wherein the output torque command includes the initial vehicle torque signal adjusted as a function of the at least a vehicle torque limit; and
generate, as a function of the output torque command, a remaining vehicle torque.