A system for distributed flight controllers for an electric aircraft is provided. The system includes a plurality of flight components coupled to the electric aircraft, a first controller coupled to an electric aircraft, the first controller configured to receive a plurality of measured aircraft data and generate a controller allocation datum as a function of the plurality of measured aircraft data. The system further includes a plurality of second controllers, wherein each second controller is configured to receive the controller allocation datum from the first controller, generate an allocation command as a function of the controller allocation datum, and provide the allocation command to each flight component of the plurality of flight components.


    Access

    Download


    Export, share and cite



    Title :

    Systems and methods for distrubuted flight controllers for redundancy for an electric aircraft


    Contributors:

    Publication date :

    2022-10-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G06N COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS , Rechnersysteme, basierend auf spezifischen Rechenmodellen