The general purpose of this study is to aid in the evaluation and design of multi-sensor navigation schemes proposed for the orbiter. The scope of the effort is limited to the post-entry, energy management, and approach and landing mission phases. One candidate system based on conventional navigation aids is illustrated including two DME (Distance Measuring Equipment) stations and ILS (Instrument Landing System) glide slope and localizer antennas. Some key elements of the system not shown are the onboard IMUs (Inertial Measurement Units), altimeters, and a computer. The latter is programmed to mix together (filter) the IMU data and the externally-derived data. A completely automatic, all-weather landing capability is required. Since no air-breathing engines will be carried on orbital flights, there will be no chance to go around and try again following a missed approach.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Space shuttle post-entry and landing analysis. Volume 1: Candidate system evaluations


    Beteiligte:
    Crawford, B. S. (Autor:in) / Duiven, E. M. (Autor:in)

    Erscheinungsdatum :

    20.07.1973


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Space shuttle post-entry and landing analysis. Volume 2: Appendices

    Crawford, B. S. / Duiven, E. M. | NTRS | 1973


    Space Shuttle Entry and Landing Navigation Analysis

    H. L. Jones / B. S. Crawford | NTIS | 1974


    Space shuttle entry and landing navigation analysis

    Jones, H. L. / Crawford, B. S. | NTRS | 1974