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.


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    Title :

    AIRCRAFT MOTION OBSERVER CONFIGURED FOR USE IN ELECTRIC AIRCRAFT


    Contributors:

    Publication date :

    2022-10-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G07C TIME OR ATTENDANCE REGISTERS , Zeit- oder Anwesenheitskontrollgeräte / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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