Systems and methods for flight control of aircraft

A computer-implemented method comprising, measuring one or more aircraft conditions;

• performing a preemptive action to dynamically vary one or more torque commands to one or more electric propulsion units based at least on the one or more aircraft conditions and using at least one of an engine or propeller characteristic to preemptively account for limitations of the one or more electric propulsion units;
• wherein the at least one of an engine or propeller characteristic comprises at least one of a rotating component inertia, an aerodynamic characteristic of a propeller, or an incidence angle of air around a propeller;
• and
• causing the one or more electric propulsion units to generate thrust based on the one or more dynamically varied torque commands from a flight control computer of an aircraft.

A non-transitory computer-readable medium storing one or more instructions that, when executed by at least one processor, cause the at least one processor to perform operations comprising:

• measuring one or more aircraft conditions;
• performing a preemptive action to dynamically vary one or more torque commands to one or more electric propulsion units based at least on the one or more aircraft conditions and using at least one of an engine or propeller characteristic to preemptively account for limitations of the one or more electric propulsion units;
• wherein the at least one of an engine or propeller characteristic comprises at least one of a rotating component inertia, an aerodynamic characteristic of a propeller, or an incidence angle of air around a propeller;
• and
• causing the one or more electric propulsion units to generate thrust based on the one or more dynamically varied torque commands.