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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Dynamic characteristics analysis of missile in ballistic flight



    Conference:

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


    Published in:

    Publication date :

    2023-12-11


    Size :

    10 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



    Free flight of ballistic missile

    Wheelon, A.D. | Engineering Index Backfile | 1959


    Optimal In-Flight Modifications of Ballistic Missile Trajectories

    Druckmann, E. / Asher, J.Z.B. / Tekhniyon, Makhon tekhnologie le-Yisra'el | British Library Conference Proceedings | 2011



    Ballistic Missile

    W. A. Mrazek | NTIS | 1966