A mathematical model of air vehicle gliding trajectory was established and attack angle was regarded as control variable. Adaptive simulated annealing algorithm was adopted to optimize the 101 nodes of attack angle. By optimizing the control law of attack angle of gliding trajectory, the maximum range of air vehicle is increased significantly, which increases 107%.


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    Titel :

    Research on Parameter Optimization Method of an Air Vehicle Gliding Trajectory



    Erschienen in:

    Advanced Materials Research ; 945-949 ; 662-665


    Erscheinungsdatum :

    06.06.2014


    Format / Umfang :

    4 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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