This thesis is an application of parameter sensitivity analysis to aerodynamic parameters of a Bank-to-Turn missile. In the development a brief review of trajectory sensitivity theory is presented. A linear analysis is performed using an Uncoupled Pitch Channel Autopilot and a Coupled Roll-Yaw Channel Autopilot of the missile taken as model. Finally, a nonlinear analysis is given for the system. Comparisons between the linear and nonlinear cases are outlined. (Author)


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    Titel :

    Application of Sensitivity Analysis to Aerodynamic Parameters of a Bank to Turn Missile


    Beteiligte:

    Erscheinungsdatum :

    1983


    Format / Umfang :

    250 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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