The requirements of a unified optimal guidance scheme are discussed, giving attention to a general formulation, aspects of self-targeting, problems of optimum guidance within the atmosphere, and a unified concept for all flight phases. Since no previous guidance scheme meets these requirements, the shuttle demands a fundamentally new approach. A new unified optimal guidance scheme, called Mascot, was developed. The capabilities of Mascot include the real-time solution of general trajectory-optimization problems and the unification of guidance for all flight phases.


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    Titel :

    Shuttle ascent guidance and control.


    Beteiligte:
    Lovingood, J. A. (Autor:in) / Blair, J. C. (Autor:in) / Geissler, E. O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    01.02.1972


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Space Shuttle Ascent Guidance, Navigation, and Control

    R. L. Mchenry / A. D. Long / B. F. Cockrell et al. | NTRS | 1979




    Space shuttle ascent aborts

    Schmidgall, R.A. | Tema Archiv | 1989