In exoatmospheric interception, steering jets is the only possible method to move a vehicle. A nonlinear vector guidance law based on a saddle-point inequality with respect to miss distance as well as capture time is presented and analyzed for both ideal and nonideal interceptors. The time to go is found to be a quartic polynomial equation, and an algebraic “first-pass” capture zone is presented. To eliminate the non-minimum-phase property of the standard thrust vector control, the paper proposes a translation without rotation interceptor configuration.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Exoatmospheric Thrust Vector Interception Via Time-to-Go Analysis


    Beteiligte:
    Gutman, Shaul (Autor:in) / Rubinsky, Sergey (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2015-07-03


    Format / Umfang :

    12 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch