Features of command type radioinertial guidance system in which ground-based radar continuously determines position of missile during powered flight and digital computer accepts data; this is done by reference to previously stored trajectory information for particular target, computing appropriate orders to maintain missile on proper flight path; corrective orders are transmitted by radio to missile and applied to missile's autopilot and control system.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Missile guidance


    Weitere Titelangaben:

    Bell Laboratories Rec


    Beteiligte:
    Felch, E.P. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1959


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Advanced missile guidance

    LAWRENCE, R. | AIAA | 1991


    Modern missile guidance

    Yanushevsky, Rafael | TIBKAT | 2019


    Predictive Missile Guidance

    R. A. Best / J. P. Norton | AIAA | 2000


    Missile Guidance Comparison

    Rogers, Steve | AIAA | 2004


    Missile guidance simulation

    Funk, J.E. / Johnson, H.D. / Schmidt, G.C. | Tema Archiv | 1984