The invention discloses a single-soldier guided
rocket dynamic target prediction and guidance method, which can effectively reduce the normal overload of a
rocket in the
flight process and ensure therelatively high hit accuracy. The single-soldier guided
rocket dynamic target prediction and guidance method comprises the following steps of: measuring the motion state of the target in a ground
inertial coordinate system by ground
fire control equipment, transforming into the
inertial coordinate system of the rocket and transmitting to a computer on the rocket; using the computer on the rocket to estimate the
flight time required for the rocket to hit the target and calculating the point of intersection of a guided
missile and the target according to the motion state of the target, the initial position of the rocket in the
inertial coordinate system of the rocket and the set speed of the single-soldier guided rocket; in the current guidance period, controlling the rocket to fly to the target point according to the set guidance law by taking the point of intersection of the guided
missile and the target as the target point; when the current guidance period ends, obtaining the positioninformation of the target in the inertial coordinate
system of the rocket by solving with the computer on the rocket, solving the remaining
flight time of the rocket hitting the target, and updatingthe point of intersection of the guided
missile and the target; and entering the next guidance period, and repeatedly executing till the rocket hits the target.