In this research, the nonlinear model of a ballistic missile has been linearized and validated. The nonlinear equation of motion for the flight dynamics of the missile has been used for modeling the missile. The transfer function and model reduction are derived. Dynamic stability analysis for longitudinal and lateral-directional motion has been made at some operating points throughout the flight. The effect of different phases and velocities of the flight has been analyzed by its pole locations and frequency response. It was found that the missile’s short period, Dutch roll, and roll subsidence mode are stable. The result of this work can be used for designing a robust autopilot controller that meets the stability and performance requirements of the plant throughout the whole flight envelope.


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    Titel :

    Dynamic characteristics analysis of missile in ballistic flight


    Beteiligte:
    Audric, Derren (Autor:in) / Fayyadh, M. S. Dzaki (Autor:in) / Sembiring, Javensius (Autor:in) / Putro, Idris Eko (Autor:in) / Septanto, Harry (Herausgeber:in) / Adhynugraha, Muhammad Ilham (Herausgeber:in) / Vetrita, Yenni (Herausgeber:in) / Santosa, Cahya Edi (Herausgeber:in) / Sitompul, Peberlin Parulian (Herausgeber:in) / Yulihastin, Erma (Herausgeber:in)

    Kongress:

    THE 9TH INTERNATIONAL SEMINAR ON AEROSPACE SCIENCE AND TECHNOLOGY – ISAST 2022 ; 2022 ; Bogor, Indonesia


    Erschienen in:

    Erscheinungsdatum :

    11.12.2023


    Format / Umfang :

    10 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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