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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    Title :

    Robust guidance law for space interception


    Contributors:
    Di Zhou, (author) / Fulian Duan, (author)


    Publication date :

    2000-01-01


    Size :

    368903 byte




    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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