Pershing II flight simulations were performed using the U70 missile simulation program to determine (1) in the event of an accidental nozzle deflection, how fast the missile would leave its (safe) flight corridor; (2) how well the U70 aerodynamic simulation matches the actual flight data; and (3) the trajectory profiles for nine Tactical Ballistic Missile flight trajectories. Also an advanced simulation program developed by TRW, Inc. was partially converted to run on an inhouse computer. (Author)
Pershing II Simulation Studies
1982
102 pages
Report
Keine Angabe
Englisch
Surface Launched Missiles , Missile Trajectories & Reentry Dynamics , Guided missiles , Air to air missiles , Validation , Ballistic trajectories , Guided missile trajectories , Flight simulators , Maximum likelihood estimation , Computerized simulation , Computer programs , Safety , Range safety , Models , Flight testing , Comparison , Flight simulation , Aerodynamics , Deflection , Nozzles , Subroutines , Flow charting , Covariance , Correlation techniques , Tables(Data) , Tactical weapons , Pershing 2 missiles , TBM(Tactical Ballistic Missiles) , U70 missile simulator , Aerodynamic coefficients
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