In an example, a computing apparatus includes a hardware platform, having a processor and a memory, and instructions encoded within the memory to instruct the processor to receive a peak power demand for a landing maneuver of a VTOL aircraft powered at least partly by a battery, receive flight profile data for a flight profile of the VTOL aircraft, and configuration data for the VTOL aircraft, estimate power consumption of the flight profile in context of the configuration, and estimate a peak power capacity available for the landing maneuver, and provide an error notice if the peak power capacity does not meet the peak power demand.


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    Title :

    ESTIMATING AVAILABLE POWER FOR AN AIRCRAFT BATTERY


    Contributors:
    FAN YUE (author) / HULL MICHAEL R (author)

    Publication date :

    2023-02-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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