Access

    Download


    Export, share and cite



    Title :

    Approximate analytical solutions for three-dimensional ascent trajectory of a solid-fuel launch vehicle with time-varying mass flow rate


    Additional title:

    Chinese Journal of Aeronautics


    Contributors:
    YU, Qi (author) / CHEN, Wanchun (author) / YU, Wenbin (author)

    Published in:

    Publication date :

    2024-10-01




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




    Approximate Analytical Solutions for Launch-Vehicle Ascent Trajectory

    Yu, Qi / Chen, Wanchun / Yu, Wenbin | IEEE | 2023


    Convex Approach to Three-Dimensional Launch Vehicle Ascent Trajectory Optimization

    Benedikter, Boris / Zavoli, Alessandro / Colasurdo, Guido et al. | AIAA | 2021


    Fuel-Optimal Ascent Trajectory Problem for Launch Vehicle via Theory of Functional Connections

    Shiyao Li / Yushen Yan / Kun Zhang et al. | DOAJ | 2021

    Free access

    Further improvements to a hybrid method for launch vehicle ascent trajectory optimization

    Calise, Anthony / Tandon, Sunil / Young, Daniel et al. | AIAA | 2000


    Modeling of Martian Ascent Launch Vehicle

    Soota, Mahima / Nadda, Sudhir | Springer Verlag | 2023