滚转发射机弹分离轨迹的仿真研究  

Trajectory Simulation of Missile Separated from Rolling Aircraft

作　　者：郑书娥[1] 

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《现代防御技术》2015年第6期32-37,130,共7页Modern Defence Technology

基　　金：航空基金(20120112002)

摘　　要：从相对运动的角度对滚转发射时机弹分离轨迹进行仿真,通过评估滚转发射时的机弹分离品质,知道机弹分离安全研究将是滚转发射时需要重点解决的技术难题,武器系统与导弹总体设计人员需要进行更深入的研究,确保载机在超机动发射时机弹安全分离,使整个武器系统以良好的性能形成战斗力。Trajectory simulation of missile separated from rolling aircraft is given on the basis of relative movement. By the safety evaluation of missile separated from rolling aircraft, the conclusion is given that missile safety separation from rolling aircraft in launch is an important technology to solve. And the weapon system and missile overall designers need thorough research to insure the separation safety so that the battle effectiveness comes into being from the excellent weapon systems.

关 键 词：滚转发射 空空导弹 机弹分离轨迹 安全分离 弹道仿真 系统设计 机动发射 

分 类 号：TJ761.1[兵器科学与技术—武器系统与运用工程] TJ760.9