An aircraft motion observer configured for use in electric aircraft includes an actuator model configured to receive at least an aircraft command, wherein the aircraft command comprises a desired change in aircraft trajectory as a function of a plurality of flight components, generate a performance datum for the flight components as a function of the aircraft command. System includes a plant model configured to generate a predictive datum for the flight components as a function of the actuator model and the performance datum. System includes a sensor communicatively connected to the aircraft configured to detect a measured state datum. System includes a controller configured to compare the predictive datum and the measured state datum, generate an inconsistency datum wherein the inconsistency datum comprises a mathematical function to compensate for the difference between the predictive state datum and the measured state datum, and transmit the inconsistency datum to the plant model.
AIRCRAFT MOTION OBSERVER CONFIGURED FOR USE IN ELECTRIC AIRCRAFT
2022-10-06
Patent
Electronic Resource
English
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