作者: Xinpeng Ma , Ruikang Xing , Xinghao Ran , Hairui Zhang
DOI: 10.1088/1757-899X/408/1/012029
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摘要: According to the multipath effect problem that missile intercepts ultra-low altitude target, when grazing angle near Brewster Angle, reflection coefficient of clutter reach minimum, and precision guidance is higher. To ensure can intercept target effectively under vertical launch condition, a super-low-altitude trajectory model established. Then an improved proportional law satisfying Angle constraint developed, overall from strike finally designed. The Simulation show designed relatively straight meets requirements. From perspective design, way solve seeker detection have been explored.