In space interception, a linear time-varying model is established to describe the missile-target related line-of-sight (LOS) motion, where the guidance parameter variations and target maneuvers are regarded as gain bounded disturbances. From this model, a robust guidance law of homing-missile is derived and its robustness against the gain bounded uncertainty is proved by Lyapunov-like approach. Simulation results obtained demonstrate the effectiveness of the presented guidance method.


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    Titel :

    Robust guidance law for space interception


    Beteiligte:
    Di Zhou, (Autor:in) / Fulian Duan, (Autor:in)


    Erscheinungsdatum :

    01.01.2000


    Format / Umfang :

    368903 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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