A new method of stability margin clearance of missile autopilot is described. First, a model of linear fractional transformation form is established for missile has uncertain parameters; then, the system stability margin requirements are seen as a virtual uncertainty and introduced into the model; Finally, the model is analyzed, and the clearance results about the missile autopilot performance is obtained. The results show this is a more efficient and accurate clearance method than traditional ones.


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    Title :

    Stability Margin Clearance of Missile Autopilot Using μ Anylysis


    Contributors:


    Publication date :

    2012


    Size :

    6 Seiten




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English