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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    Title :

    Determination of take-off constraints for the aerospace vehicle


    Contributors:
    Rui, Cao (author) / Feiteng, Jin (author) / Huimin, Su (author) / Wenjie, Wang (author) / Yanbin, Liu (author) / Yuping, Lu (author)


    Publication date :

    2018-08-01


    Size :

    255456 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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