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)
Tactical Missile Encounter (TAME) Simulation Computer Program. Volume 2. Users Manual
1970
32 pages
Report
No indication
English
Missile Trajectories & Reentry Dynamics , Computer Hardware , Air to air missiles , Guided missile trajectories , Computer programming , Guided missile models , Guided missile targets , Flight paths , Simulation , Miss distance , Angle of attack , Automatic pilots , Aerodynamic characteristics , Control sequences , Subroutines , Computer analysis , Computerized simulation , Tactical missile encounter , Tame computer program , Tame(Tactical missile encounter) , Three degrees of freedom , S/L change 8411
TIBKAT | 1996
|NTRS | 1986
|AIAA | 2003
|