The benefits of relaxed static stability on missile were examined. Based on optimal control and open-loop crossover frequency constraint, an acceleration autopilot design methodology was developed and applied to a highly unstable airframe. Performance and robustness comparisons for three autopilot topologies were made. The analysis reveals the topology origin of classic three-loop autopilot, and simulation results show that the four-loop topology looks very promising.


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    Titel :

    Missile autopilot design using optimal control and frequency constraint


    Beteiligte:
    Fan, Jun-fang (Autor:in) / Lin, De-fu (Autor:in) / Qi, Zai-kang (Autor:in) / Wang, Jiang (Autor:in)


    Erscheinungsdatum :

    01.12.2008


    Format / Umfang :

    524785 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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