Guidance method is described for lifting maneuverable vehicle through atmospheric entry from end of survival phase to point where ground based guidance or pilot assumes control for landing phase; method makes it possible to guide entering vehicle explicitly using paths other than equilibrium glide (constant lift/drag) path segments; arbitrary specification of initial conditions can be made, and both velocity and altitude, as well as range and cross range, can be specified at beginning of final landing phase; simulation results.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Exponential reentry guidance


    Weitere Titelangaben:

    IEEE -- Tech Paper


    Beteiligte:
    Kirby, M.J. (Autor:in) / Klein, R.L. (Autor:in)

    Kongress:

    12th IEEE East Coast Conference on Aerospace and Navigational Electronics ; 1965 Re-entry


    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Reentry guidance for Space Shuttle

    Causey, W. / Sohoni, V. | NTRS | 1973



    Gemini reentry guidance and control system

    Paddock, Jr., S.G. | Engineering Index Backfile | 1966


    Atmospheric Reentry Guidance of Manned Spacecraft

    Wang, Z. / Han, C. / Beijing University of Aeronautics and Astronautics | British Library Conference Proceedings | 1994


    A GUIDANCE SCHEME FOR LIFTING REENTRY

    TERASAKI, RICHARD | AIAA | 1963