A control system of permanent magnet synchronous motor ensuring its fail-safety at the expense of switchover between several scalar control modes, is proposed. A computer simulation model is realized. The operation of such a system is analyzed in terms of the electric pump unit of space application.


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    Title :

    Fail-Safe Control System for an Electric Pump Unit of Space Application


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 64 , 2 ; 210-218


    Publication date :

    2021-04-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English





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