The space shuttle digital, fly by wire, flight control system presents an interesting challenge in avionics system design. In residence in each of four redundant general purpose computers at lift off are the guidance, navigation, and control algorithms for the entire flight. The mission is divided into several flight segments: first stage ascent, second stage ascent; abort to launch site, abort once around; on orbit operations, entry, terminal area energy management; and approach and landing. The FCS is complicated in that it must perform the functions to fly the shuttle as a boost vehicle, as a spacecraft, as a reentry vehicle, and as a conventional aircraft. The crew is provided with both manual and automatic modes of operations in all flight phases including touchdown and rollout.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space shuttle digital flight control system


    Beteiligte:
    Minott, G. M. (Autor:in) / Peller, J. B. (Autor:in) / Cox, K. J. (Autor:in)


    Erscheinungsdatum :

    1976-08-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space Shuttle flight control system

    Klinar, W. J. / Kubiak, E. T. / Peters, W. H. et al. | NTRS | 1975


    Space Shuttle on-orbit flight control system

    NAKANO, M. / WILLMS, R. | AIAA | 1982


    Space Shuttle flight operations.

    Carlton, R. L. | NTRS | 1973



    Large Space Shuttle Flight Experiment

    Jenkins, L. M. | NTRS | 1982