现代防御技术2012，Vol.40Issue(3)：44-49,6.DOI:10.3969/j.issn.1009-086x.2012.03.009
俯冲击顶弹道落角研究
Impact Angle of Upper Attack Trajectory
摘要
Abstract
A larger impact angle is needed to guarantee the damage effect of the missile when upper attack trajectory is adopted. To increase the impact angle and damage effect of upper attack trajectory, the influences on impact angle are analyzed from the aspects of range and height of trajectory, turning over point and coefficient of proportional navigation, and available normal overload respectively. Moreover, measures to increase the impact angle are proposed such as adjusting launch angle, adopting thrust vector control and improving terminal guidance law. Simulation and citation references show that the impact angle can be increased effectively with these measures.关键词
飞行力学/俯冲击顶/落角Key words
flight mechanics (dynamics) / upper attack/ impact angle分类
军事科技引用本文复制引用
高峰,唐胜景,师娇..俯冲击顶弹道落角研究[J].现代防御技术,2012,40(3):44-49,6.
