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.


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    Titel :

    Singular Perturbation Guidance of Hypersonic Glide Reentry


    Beteiligte:
    Chen, Wanchun (Autor:in) / Zhou, Hao (Autor:in) / Yu, Wenbin (Autor:in) / Yang, Liang (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2020-11-08


    Format / Umfang :

    20 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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