Proportional navigation (PN) has attracted a amount of interest in the missile interception and continues to be a benchmark for new missile guidance laws due to the high effectiveness and simple implementation [87, 285, 97, 248]. It is well known that PN is the optimal guidance law with a navigation ratio N = 3, and it can result in successful interceptions under a wide range of engagement conditions. However, the PN guidance law is more applicable for the task of intercepting a non-maneuvering target or a weakly maneuvering target. In practice, target acceleration can change rapidly. For intercepting a target with powerful maneuvering capability, the performance of PN is degraded and it may be ineffective for some orientations between missile and target.


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    Title :

    Missile Guidance Law Based on ESO Techniques


    Additional title:

    Lect.Notes Control


    Contributors:
    Xia, Yuanqing (author) / Fu, Mengyin (author)


    Publication date :

    2013-01-01


    Size :

    18 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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