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 this volume 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. (Author)


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    Tactical Missile Encounter (TAME) Simulation Computer Program. Volume 2. Users Manual

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



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