Optimal evasion against a persuer guided by the proportional navigation method (Q5936684)

The authors study the problem of determining the trajectory of optimal evasion from the persuer directed by the method of proportional navigation. It is assumed that the object and the missile are moving in a plane and are material points, the point velocities are constant, there is no delay in the system and the method of proportional guidance is realized ideally on the missile. The domain of the initial conditions is specified under which the object necessarily evades the missile.