A compensation scheme is presented for the pitch-yaw control system of a strategic missile which maintains stability and performance while the missile spins. The conventional missile control design for boost has uncoupled pitch, yaw and roll channels ideally suited for a non-rolling missile. The effect roll has on the conventional pitch-yaw controller is discussed and the development and simulation of a modified system is presented. Keywords: Spinning missile; and Thrust vector control.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Boost Control Design for Spinning Missile


    Beteiligte:
    R. L. Park (Autor:in)

    Erscheinungsdatum :

    1985


    Format / Umfang :

    97 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Boost Assisted Missile Launcher

    L. J. Holt / C. Panlaqui | NTIS | 1979


    Vacuum-air missile boost system

    KUMAR, S. / MURRAY, J. J. / RAJAN, J. R. N. | AIAA | 1964




    Midcourse Guidance and Control for Pulse Motor Boost Missile

    Tang, Mao / Gong, Yinghui / Xie, Jia et al. | Springer Verlag | 2021