Guidance Trajectory Simulation of the Three Points Method of Antitank Missile

Guidance law is the rule that missile centroid motion follows,that determines space moving trace of trajectory centroid.In missile guidance system,function of guidance law is that it determines trajectory of missile flying and attacking target in kinematics.How appropriate guidance method is taken to improve performance of missile guidance and precision of the missile hitting are cared still.Guidance Trajectory of the three points method is studied.Parameters that effect guidance Trajectory are analyzed.Merits and demerits of the three points method are summarized.And subjects are taken.