Two algorithms were developed to demonstrate the implementation of autonomous functions in an existing spacecraft power system. The functions selected for autonomous operation include a typical performance monitoring function, battery state of charge, and a fault detection and response function represented by a battery state of charge below a preselected limit. The constraints imposed by the existing power system configuration are the available data in the telemetry stream and the existing commands and command structure. The areas requiring future development are the degree of battery characterization, the effects of hardware/software faults, and the verification of faults.


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    Title :

    Algorithm development for a spacecraft autonomous power system


    Additional title:

    Entwicklung eines Algorithmus fuer ein autonomes Energiesystem in einem Raumschiff


    Contributors:


    Publication date :

    1983


    Size :

    5 Seiten, 5 Bilder, 2 Tabellen, 5 Quellen


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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