The hinge moment acting on the actuator will cause an out-of-plane moment, which is a destabilizing factor to the angular motion of spinning missiles. A new tuning criterion for the actuator controller is proposed to decrease the out-of-plane moment. It is noted that the integral element does not decrease the out-of-plane moment. A carefully designed proportional–derivative controller with some compromises can ensure the stability of the missile and provide good performance for the actuator.


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    Titel :

    Retuning the actuator proportional–integral–derivative controller of spinning missiles


    Beteiligte:
    Zhou, Wei (Autor:in) / Yang, Shuxing (Autor:in) / Zhao, Liangyu (Autor:in)


    Erscheinungsdatum :

    01.12.2017


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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