Patent attributes
A system and method for flight control compensation for component degradation is illustrated. The system comprises a first flight component mechanically coupled to the electric aircraft and a second flight component mechanically coupled to the electric aircraft. A sensor is also coupled to both the first flight component and the second flight component, wherein the sensor is configured to detect a performance degradation datum in one of the first flight component and the second flight component and transmit the performance degradation datum to a flight controller. The system also comprises a flight controller communicatively coupled to the sensor, wherein the flight controller is configured to receive the performance degradation datum from the sensor and adjust operation of either the first flight component or the second flight component as a function of the performance degradation datum.