An angle-of-attack control system for Hypersonic Reentry Vehicle driven by Reaction Control System (RCS) is designed based on Phase Plane Method (MPPM) in this paper. Firstly, the model of Hypersonic Reentry Vehicle and the RCS model are introduced. Then the design method for the modified phase plane controller is presented in detail. Finally, the performance of the designed controller is demonstrated by simulation with linear model of Hypersonic Reentry Vehicle, which shows that the effectiveness and rationality of the modified phase plane controller.


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    Titel :

    Control system design for Hypersonic Reentry Vehicle driven by RCS based on modified Phase Plane Method


    Beteiligte:
    Liang, Dong (Autor:in) / Song, Jian-mei (Autor:in) / Cai, Gao-hua (Autor:in)


    Erscheinungsdatum :

    01.07.2013


    Format / Umfang :

    287345 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch