制导火箭弹射表编拟研究  

Research on Compilation of Firing Tables of Guided Rocket

作　　者：杨明 高宏伟 汤祁忠 

机构地区：[1]中国兵器工业导航与控制技术研究所,北京100089

出　　处：《火力与指挥控制》2013年第12期156-159,共4页Fire Control & Command Control

摘　　要：将制导控制技术应用于多管火箭系统,解决了火箭弹射程与精度相互制约的矛盾,实现了射程与精度的同步提升,并赋予火箭弹一定的变轨控制能力。针对制导火箭弹弹道设计及射表编拟中出现的新课题,对制导火箭弹的控制能力进行了分析,结合制导火箭弹的使用特点,给出了制导火箭弹射表编拟的技术实现途径,讨论了制导火箭弹的弹道高程限制和标准化射程的设计依据。The contradictory between range and precision have been solved since guidance and control technology are used to multiple rockets system,and the guided rocket has been promoting the ability of maneuvering and orbit changing. To design compilation of firing tables, the control ability of the guided rocket is analyzed,and trajectory and standardization range the technical method of compilation is given. The ceiling of the of the guided rocket are also discussed.

关 键 词：制导火箭弹 射表 编拟 标准化射程 发射诸元 

分 类 号：TJ765.3[兵器科学与技术—武器系统与运用工程] TJ393