防空武器模拟动态飞行试验方法  

New Method of Dynamic Flight Simulation Experiment for Anti-aircraft Weapon

作　　者：丁天宝[1] 杨东[1] 何朝[1] 王琨[1] 

机构地区：[1]西北机电工程研究所,陕西咸阳712099

出　　处：《兵工学报》2016年第3期408-413,共6页Acta Armamentarii

基　　金：西北机电工程研究所预先研究项目(2014-01-FJ1335)

摘　　要：为解决防空武器模拟动态飞行试验问题,提出了防空武器模拟动态飞行试验系统工作原理和方法,建立了模拟动态飞行试验目标真值数学模型、稳定试验摇摆量真值数学模型。通过某典型防空武器系统模拟动态飞行试验验证,证明了模拟动态飞行试验原理和所建立的数学模型的正确性。该方法建立了防空武器动态飞行试验系统的理论基础,模型可用于模拟动态飞行试验数据处理和误差分析。A new principle of dynamic flight simulation experiment for anti-aircraft weapon is presented for the simulation experiment of anti-aircraft weapon in laboratory. A mathematical model of obtaining the tagart truth values and a mathematical model of obtaining the truth values of pitch and roll positions of tracker are established. The dynamic flight simulation experiment principle and the mathematical models are verified through dynamic flight simulation experiment. The principle and the key technologies of simulating dynamic flight experiment are valuable for dynamic flight simulation experiment of anti-aircraft weapons,which will promote the research and development of new anti-aircraft weapons. The proposed method is used to establish the theoretical basis of the dynamic flying experimental system,which can be used for data processing and error analysis.

关 键 词：兵器科学与技术 防空武器 动态飞行试验 真值 

分 类 号：TJ301[兵器科学与技术—火炮、自动武器与弹药工程]