Modeling of Missile Launch Point and Burnout Point Estimation Function of Early Warning Satellite System

Abstract

Early warning satellite system is on the front edge of ballistic missile defense system, and plays an important role in leading other early warning systems and interceptor systems. Based on trajectory characteristic and polynomial fitting method, ballistic missile launch point parameters estimation model and burnout point parameters estimation model are built, and a classical case of American early warning satellite system is simulated and analyzed, and the validity of the models is shown by the result.