A comparison of two different autopilot configurations and their effect on missile response is presented. The comparison includes the steps taken in determining missile parameters from wind tunnel data and flight condition data. The missile parameters are coupled with two different autopilot configurations to determine any significant advantage of one configuration over the other. Pole placement is used in determining required autopilot feedback and feed forward gains. Simulations of each autopilot are conducted and the responses are compared. Keywords: Military thesis. (KT)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Effect of Autopilot Configuration on Missile Response


    Beteiligte:

    Erscheinungsdatum :

    1989


    Format / Umfang :

    75 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Effect of Missile Configuration and Inertial Measurement Unit Location on Autopilot Response

    Stein, Nitai / Weiss, Haim / Hexner, György et al. | AIAA | 2016


    The Combined Effect of Missile Configuration and IMU Location on the Autopilot Response

    Stein, N. / Weiss, H. / Hexner, G. et al. | British Library Conference Proceedings | 2013


    Robust Nonlinear Missile Autopilot Design

    McFarland, M. B. / D'Souza, C. N. / International Federation of Automatic Control | British Library Conference Proceedings | 1995


    Hybrid BTT/STT missile autopilot design

    Bai, Chengchao / Lu, Fei / Xu, Xibao | Emerald Group Publishing | 2017