Mathematical Modeling of Aerodynamic Space -to - Surface Flight with   Trajectory for Avoid Intercepting Process
  Modeling has been created for a Space-to-Surface system defined for an optimal trajectory for targeting in terminal phase with avoids an intercepting process. The modeling includes models for simulation atmosphere, speed of sound, aerodynamic flight and navigation by an infrared system. The modeling and simulation includes statistical analysis of the modeling results. 
Serge Gornev