In order to solve the dynamics and kinematics highly coupled problem which exists in missile separating from cavity and in order to acquire accurate trajectory parameters and import control system, a parallel collaborative simulation platform was established. The data interface between FLUENT and SIMULINK was developed by the way of share data file, which use the Journal file of FLUENT and S-function of SIMULINK. The missile’s rudder control model was established. The aerodynamics characters and trajectory characters during missile separating from cavity were simulated under uncontrolled and closed-loop controlled conditions. The simulation results verify the feasibility of parallel collaborative simulation and show that rudder control method can effectively improve the characteristics of missile separating from cavity.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    FLUENT/SIMULINK Collaborative Simulation for Missile Separation from Cavity


    Beteiligte:
    Han, Tong (Autor:in) / Tang, Shang-Qin (Autor:in) / Huang, Chang-Qiang (Autor:in) / Dong, Kang-Sheng (Autor:in)


    Erscheinungsdatum :

    2012


    Format / Umfang :

    5 Seiten




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    FLUENT/SIMULINK Collaborative Simulation for Missile Separation from Cavity

    Han, Tong ;Tang, Shang Qin ;Huang, Chang Qiang | Trans Tech Publications | 2012


    A Collaborative Guidance and Control Method Based on Simulink Simulation

    Gong, Yudong / Li, Jianhua / Li, Hongtao et al. | IEEE | 2023



    The Simulation of Submarine-Launched Missile Out-Water Movement Based on MATLAB/Simulink

    Lian, Yong Qing ;Tian, Bing ;Wang, Shu Zong | Trans Tech Publications | 2012


    Fluent releases Version 5.0 FLUENT software

    Emerald Group Publishing | 1999