Aiming at the Common Aero Vehicle (CAV) entry guidance problem under various trajectory constraints and terminal conditions, an on-board reference trajectory generation method was proposed, and then linear quadratic regulator (LQR) was designed to track the longitudinal reference trajectory. Lateral guidance was realized by using bank-reversal strategy with the aid of the azimuth error corridor. Finally, the entry trajectory was presented based on the above method.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Entry guidance for Common Aero Vehicle


    Beteiligte:
    Zhou Wenya, (Autor:in) / Chen Hongbo, (Autor:in) / Yang Di, (Autor:in)


    Erscheinungsdatum :

    01.12.2008


    Format / Umfang :

    537624 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Constrained predictor corrector entry guidance for common aero vehicle

    Haoliang, Wang / Yongzhao, Hua / Qingdong, Li et al. | IEEE | 2015




    Adaptive guidance for an aero-assisted boost vehicle

    Pamadi, Bandu N. / Taylor, Lawrence W., Jr. / Price, Douglas B. | NTRS | 1990


    Adaptive guidance for an aero-assisted boost vehicle

    PAMADI, BANDU N. / TAYLOR, LAWRENCE W. / PRICE, DOUGLAS B. | AIAA | 1990