火药脉冲助推器控制在舰载火箭弹中的应用  

Application of impulse thruster control on shipborne rocket

作　　者：邓大新[1] 周曾素[1] 

机构地区：[1]海军工程大学兵器工程系,湖北武汉430033

出　　处：《海军工程大学学报》2002年第4期62-67,共6页Journal of Naval University of Engineering

摘　　要：建立了采用火药脉冲助推器控制的简易制导火箭弹的弹道模型 ,进行了数字仿真 .理论研究和数字仿真结果表明 ,采用火药脉冲助推器控制可以有效地提高火箭弹的命中精度 ,它对实际弹道修正的效果与其冲量大小、数目、作用起始时刻、作用方位角。The ballistic trajectory model of simply guided rocket projectile controlled by impulse thruster is put forward, some key points are analyzed, numerical simulation is introduced. The theoretical research and numerical simulation results show that the application of impulse thruster control can effectively improve the hit probability of rocket, and the correction result has relation to its impulse value, number, starting time, azimuth, time interval, and so on.

关 键 词：火药脉冲助推器控制 舰载火箭弹 建模 仿真 

分 类 号：TJ415[兵器科学与技术—火炮、自动武器与弹药工程]