PROCEDURE TO IMPROVE THE TARGETING ACCURACY OF A DIRECTED MISSILE.

摘要

IT IS A PROCEDURE TO IMPROVE THE ACCURACY OF IMPACT OF A BODY THAT FLIES PROGRAMMALLY, THROUGH DISTURBANCES OF THE ORBIT. WHEREAS, THE DESIRED ORBIT OF THE FLIGHT ELEMENT, ACCELERATED IN THE FINAL PHASE, BEFORE AND DURING ACCELERATION, IS EQUIPPED WITH ORBITAL PREDICTION MEANS, TO COMPENSATE THE DISTURBANCES OF THE FLIGHT ORBIT.