Systems and methods for flight control system using simulator data

A method for flight control system using simulator data for an electric aircraft, the method comprising:

• receiving, by a computing device, a plurality of measured flight data comprising a desired command;
• simulating a plurality of aircraft performance model outputs as a function of the plurality of measured flight data;
• generating, by the computing device a plurality of expected aircraft performance model outputs;
• identifying, by the computing device, a malfunctioning flight component of the electric aircraft as a function of the plurality of measured flight data and the a plurality of expected aircraft performance model outputs, wherein identifying the malfunctioning flight component comprises:
• sorting, by the computing device, the plurality of expected aircraft performance model outputs based on similarity to the measured flight data;
• determining by the computing device, a moment datum, wherein the moment datum is determined as a function of at least the desired command of the plurality of measured flight data and the plurality of expected aircraft performance model outputs and comprises a plurality of prioritization data, the plurality of prioritization data comprising a prioritization datum corresponding to each of the plurality of aircraft performance model outputs;
• generating by the computing device, an allocation command datum as a function of the moment datum and the plurality of aircraft performance model outputs;
• and
• performing by the computing device, a torque allocation on a flight component of a plurality of flight components as a function of the allocation command datum and the moment datum.