The invention provides a
missile interception
system, and relates to the technical field of
missile interception, through reasonable
layout and clear division of labor of three
radar stations A, B and C. A point A is responsible for initial detection and
data transmission, a point B is responsible for launching an interception
missile, and a point C is responsible for short-distance accurate command, so that the interception success rate is increased; ground projection point coordinates are measured through
laser ranging and
radar reflection
waves, the distance between an enemy
satellite and the ground and a flight path equation are calculated through the triangle principle, parameters form a
sky buoy equation, accurate guidance is provided for interception, the distance between a point A and a point B is 830 kilometers,
data transmission and missile launching time is ensured, and the interception efficiency is improved. The point A transmits a
parameter equation to the point B and the point C after identifying the enemy
satellite, the point B launches a missile and reminds the point C, the point C receives the command right after finding the missile, interference is avoided, when the enemy
satellite flies again, the point B and the point C have more preparation time, and the interception rate is further increased.