Moving target such as Intercontinental Ballistic Missile is to be hit by interceptor after latter has completed its power-flight maneuver; it is assumed that only control available for guidance of interceptor missile is normal acceleration due to aerodynamic lift force; problem is to find "best" strategy, i.e., "best " time history of normal acceleration; optimization problem is defined leading to earliest interception; results are given and mathematical derivations can be found in appendix.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimal aerodynamic steering for anti-ICBM missiles


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    Halkin, H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1965


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Defence against ICBM

    Billington, I.J. / Cole, A.L. / Lamb, B.S. | Engineering Index Backfile | 1956


    ICBM inertial guidance

    Goetz, E.A. | Engineering Index Backfile | 1958


    Athena reproduces ICBM dynamics

    Kaufman, A. | Engineering Index Backfile | 1964


    Anti-ICBM intercept guidance for better kill probability

    Hays, S.D. | Engineering Index Backfile | 1960


    Air mobile ICBM systems

    PLYMALE, B. | AIAA | 1974