A simulation of the Skylab attitude and pointing control system (APCS) is outlined and discussed. Implementation is via a large hybrid computer and includes those factors affecting system momentum management, propellant consumption, and overall vehicle performance. The important features of the flight system are discussed; the mathematical models necessary for this treatment are outlined; and the decisions involved in implementation are discussed. A brief summary of the goals and capabilities of this tool is also included. (Author)


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    Titel :

    A Computer Simulation of Skylab Dynamics and Attitude Control for Performance Verification and Operational Support


    Beteiligte:
    H. Buchanan (Autor:in) / D. Nixon (Autor:in) / R. Joyce (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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