防空多管火箭武器跟踪发射模型研究  

Study on Launch Model of Multiple Launch Rocket System for Air Defense While Tracking Target

作　　者：任杰[1] 马大为[1] 朱忠领[1] 朱孙科[1] 

机构地区：[1]南京理工大学机械工程学院,江苏南京210094

出　　处：《火炮发射与控制学报》2012年第2期79-83,共5页Journal of Gun Launch & Control

摘　　要：立足于火箭武器发展的需求,研究了防空多管火箭炮的跟踪运动对火箭弹离轨参数的影响,给出了跟踪发射时火箭弹运动参数的计算方法,确定了火箭弹脱离定向器瞬时的运动参数,获得了空间弹道计算的初始条件,同时研究了两种特殊跟踪运动下火箭弹的离轨参数,为火箭弹飞行性能优化和发射装置的设计提供了参考。To face the development of rocket weapons,this article was focused on the rocket lift-off parameters of multiple launch rocket system for air defense while tracking target.The formulas of lift-off parameters were developed when the rocket was launched in the tracking mode,and the run-off the track parameters of rocket were determined,then the initial trajectory parameter of the rocket which is the initial condition of rocket exterior ballistics can be calculated.Also the rocket lift-off parameters of two special tracking movement were studied.It can be used as a reference for the design and optimization of ro-cket flying performance and rocket launcher.

关 键 词：基础力学 多管火箭 跟踪 发射模型 离轨参数 

分 类 号：TJ71[兵器科学与技术—武器系统与运用工程]