A new trajectory design approach for lift-control reentry flight vehicle based on cruising design concept is proposed in this paper. The cruising parameter could be aerodynamic overload, dynamic pressure, or aeroheating rate at stagnation point. For a high speed reentry flight vehicle, based on this trajectory design approach, it could firstly cruise at an appropriate aeroheating rate, then at an appropriate aerodynamic overload, and finally at an appropriate dynamic pressure. As an example, the entry trajectories designed for a certain lift-control reentry vehicle based on the new approach are presented in this paper, too.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A New Reentry Trajectory Design Approach for Lift-control Flight Vehicle Based on Cruising Design Concept


    Beteiligte:
    Zhengchun, He (Autor:in)


    Erscheinungsdatum :

    01.08.2018


    Format / Umfang :

    408989 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Trajectory control for a low-lift maneuverable reentry vehicle

    ROENNEKE, AXEL / CORNWELL, PHILLIP | AIAA | 1992


    Nonlinear flight control for a high-lift reentry vehicle

    Roenneke, Axel / Well, Klaus | AIAA | 1995


    Flight Design CT: Cruising Total

    Online Contents | 1997


    Adaptive Fuzzy Sliding Mode Control Design for a Low-Lift Reentry Vehicle

    Ghasemi, A. / Moradi, M. / Menhaj, M. B. | ASCE | 2011