Research Oh Midcourse Maneuvering Penetration Guidance Law of Ballistic Missile Based on Genetic Algorithm

The maneuvering penetration guidance law in the middle-course flight of the strategic missile is developed by simulation method in this paper A maneuvering penetration scheme based on detect system is presented and researched Based on calculation to maneuvering penetration time with Genetic Algorithm, a new type of optimal penetration guidance law is presented The optimal, earliest and latest maneuvering penetration time calculating optimization models are designed Finally, the penetration- interception simulated system based on those Models is built, the simulation experiments show the guidance law feasible and effective and its results are analyzed