基于脉冲响应的伴随方法在导弹制导性能评估中的应用  

Adjoint Technique Based on Impulse Response in Missile Performance Evaluation

作　　者：杨鹏锐[1] 张威[1] 

机构地区：[1]中国空空导弹研究院,洛阳471000

出　　处：《计算机与数字工程》2017年第7期1461-1463,共3页Computer & Digital Engineering

摘　　要：工程实现阶段,评估导弹性能的方法中直接的数学仿真最为准确,但此种方式仿真工作量大。在设计初期,弹内分系统模型尚不准确,无法准确海量仿真。论文通过对原始导弹系统建立伴随模型的方法,极大减小了系统仿真工作量,且对于多个输入,可以快速对比系统最终输出对所有输入的敏感程度。Missiles9 performance in implementation is always evaluated from direct simulating results, which cost heavy work-load. Accurate simulation at the beginning is not got due to the variations of components. Adjoint model based on the primitive seek-er loop decreases workload on emulation considerably. Comparisons of output from inputs, which reflects sensitivity of the system, can be easily obtained.

关 键 词：伴随模型 寻的回路 仿真 

分 类 号：TJ765[兵器科学与技术—武器系统与运用工程]