Design of Guided Air Ammunition＇s Optimal Guidance Law
摘要
Some long distance air ammunition can be used to attack large still target. According to this character and according to the mathematical description of target-missile relative motion built by the message supplied by the strapdown inertial navigation system/global position system (SINS/GPS) of air ammunition, optimal guidance law is designed by applying optimal control theory. The simulation is provided to indicate that when the air ammunition reaches the target, its line-of-sight (LOS) and LOS angular rate can nearly equal zero. So the air ammunition can get good terminal attitude, and the air ammunition reaches the target at the expected velocity and heading.
引用本文（GB/T 7714）
刘敏, 刘藻珍, 王保成. Design of Guided Air Ammunition＇s Optimal Guidance Law[J]. 北京理工大学学报：英文版, 2005.
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