Aiming at the problem of cooperative guidance and control of exoatmospheric multi interceptors. Firstly, based on the idea of formation flight, a multi-compound cooperative guidance strategy based on Lambert guidance, Hill guidance and line-of-sight guidance is proposed. Then, aiming at the collision avoidance problem of multiple interceptors, the minimum distance control method of orbit surface based on Hill guidance strategy is designed. Finally, for the realization of velocity gain of the above two guidance methods, a velocity gain realization method based on energy optimization is proposed.


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    Titel :

    Research on Cooperative Guidance and Control Method of Exoatmospheric Multi Interceptors


    Beteiligte:
    Li, Hongyu (Autor:in) / Dun, Xiaobiao (Autor:in) / Yin, Tong (Autor:in) / Cai, Jingzhu (Autor:in)


    Erscheinungsdatum :

    15.10.2021


    Format / Umfang :

    29421773 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch