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.


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    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 :

    01.08.2018


    Format / Umfang :

    255456 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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