Since inverter induced instability is system problem, analysis of whole aircraft d-c power system is presented to point out measurable properties which may be used to predict stability. (See also Am Inst Elec Engrs -- Trans v 76 (Applications and Industry) n 32 Sept 1957 p 183-8)


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    Title :

    Stability of aircraft D-C power systems with inverter loads


    Additional title:

    Elec Eng


    Contributors:

    Published in:

    Publication date :

    1957


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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