A preliminary design of the Cassini Thrust Vector Control algorithm which controls the spacecraft attitude during main engine burns is described. The discussion includes software architecture, sensor/actuator characteristics, and vehicle dynamics, as well as controller design and margin analysis via clasical methods, and performance evaluation via simulation.


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    Titel :

    Thrust Vector Control Algorithm Design for the Cassini Spacecraft


    Beteiligte:

    Erscheinungsdatum :

    17.02.1993


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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