The factors leading to the particular design of the Shuttle guidance, navigation and control software are discussed. The derivation of explicit guidance equations satisfying a wide range of different maneuver constraints and steering equations that create attitude steering errors from the guidance solutions is presented, as are navigation equations, and equations for identifying faulty instruments from sets of redundant instrument measurements.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space Shuttle Ascent Guidance, Navigation, and Control


    Beteiligte:
    R. L. Mchenry (Autor:in) / A. D. Long (Autor:in) / B. F. Cockrell (Autor:in) / J. R. Thibodeau, III (Autor:in) / T. J. Brand (Autor:in)


    Erscheinungsdatum :

    1979-03-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Shuttle ascent guidance and control.

    Lovingood, J. A. / Blair, J. C. / Geissler, E. O. | NTRS | 1972



    Space shuttle ascent aborts

    Schmidgall, R.A. | Tema Archiv | 1989