Trajectory optimization of high-speed kinetic energy anti-tank missile with pulse correction

High speed kinetic energy antitank missile is an important development direction of antitank weapons in the future. Aiming at the high-speed kinetic energy antitank missile system with pulse correction engine as actuator and three-point guidance scheme, a trajectory optimization method in the lead-in phase is designed, which can be applied in engineering. Firstly, the principle and mathematical model of the pulse correction high-speed kinetic energy antitank missile system are described in detail. Then, the trajectory optimization scheme of the pulse correction high-speed kinetic energy missile in the lead-in phase is described, and the trajectory optimization model is established. Then, taking a certain type of high-speed kinetic energy missile as an example, the trajectory optimization scheme of the lead-in phase is verified and analyzed by mathematical simulation. The real results show that the designed trajectory optimization algorithm can effectively reduce the pulse energy consumption in the lead-in phase.