The two volumes of this document present an analyst manual and a users manual for a three dimensional, three degree-of-freedom trajectory simulation. The missile model described in Volume 1 uses trimmed aerodynamic data (zero pitching moment) with the missile autopilot computations approximated in the steady state using a single time lag representation of the dynamic response. Several missile autopilot systems are approximated as are several target options. Input instructions and explanations of the output are contained in this volume. (Author)


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    Tactical Missile Encounter (TAME) Simulation Computer Program. Volume 1. Analyst Manual

    D. R. Peters / R. D. Feldman / H. Sobel et al. | NTIS | 1970



    Tactical missile propulsion

    Jensen, Gordon E. | TIBKAT | 1996


    Tactical missile aerodynamics

    Hemsch, Michael J. / Nielsen, Jack N. | NTRS | 1986


    Advancved Tactical Missile

    Paul, S. / Frederick, R. / Davis, C. | AIAA | 2003