A drive system for an electrically-driven aircraft can include a first motor controller and a second motor controller. The first motor controller can control a motor to propel a vehicle housing. The first motor controller can control the motor using a parameter measured with a sensor that is configured to monitor a motor system component. The second motor controller can control the motor in place of the first motor controller to propel the vehicle housing. The second motor controller can control the motor without using a physical position and a change in the physical position of any motor system component measured with any sensor.


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    Title :

    DRIVE SYSTEM FOR ELECTRICALLY-DRIVEN AIRCRAFT


    Contributors:

    Publication date :

    2020-07-23


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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