In the previous chapter, the trajectory optimation for maximum range of hypersonic glider with no constraints has been finished by collocation method and sequential quadratic programming method. Then, a guidance law can be designed for tracking the optimal trajectory. However, in practice, the off-line calculations are very time consuming, and the original optimal trajectory may lose its optimality due to the changes in flight conditions caused by various disturbances or unexpected external forces.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Singular Perturbation Guidance of Hypersonic Glide Reentry


    Contributors:
    Chen, Wanchun (author) / Zhou, Hao (author) / Yu, Wenbin (author) / Yang, Liang (author)

    Published in:

    Publication date :

    2020-11-08


    Size :

    20 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




    Trajectory Damping Control Technique for Hypersonic Glide Reentry

    Chen, Wanchun / Zhou, Hao / Yu, Wenbin et al. | Springer Verlag | 2020


    Steady glide trajectory planning method for hypersonic reentry vehicle

    Hu, Jinchuan / Chen, Wanchun | British Library Online Contents | 2015


    A Cooperative Reentry Trajectory Optimization Method for Hypersonic Glide vehicles

    Li, Xiaoxuan / Jiang, Zhanyuan / Ge, Jianquan et al. | IEEE | 2021