This paper studies the conditions of the successful takeoff and climbing of the aerospace vehicle. By analyzing the longitudinal kinematics model and dynamic model of the vehicle, the take-off constraints determined by integrating with the lift-drag ratio, thrust-to-weight ratio, flight speed and take-off weight. Moreover, the algebraic form of the maximum take-off weight is also derived to ensure that the aircraft can successfully take off under a fixed configuration. Finally, the simulation results verify the effectiveness of the proposed methods.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Determination of take-off constraints for the aerospace vehicle


    Beteiligte:
    Rui, Cao (Autor:in) / Feiteng, Jin (Autor:in) / Huimin, Su (Autor:in) / Wenjie, Wang (Autor:in) / Yanbin, Liu (Autor:in) / Yuping, Lu (Autor:in)


    Erscheinungsdatum :

    2018-08-01


    Format / Umfang :

    255456 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Galaxy Aerospace to Take Over

    Gilbert, G. A. | British Library Online Contents | 1997


    Aerospace vehicle

    Jackson, L. R. / Taylor, A. H. | NTRS | 1985


    Aerospace Vehicle

    L. R. Jackson / A. H. Taylor | NTIS | 1984


    Wiring Aerospace Vehicle

    SAE Technical Papers | 2019


    Wiring Aerospace Vehicle

    SAE Technical Papers | 2010