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复合制导空空导弹快速仿真研究与应用
引用本文:任宏光,周桢.复合制导空空导弹快速仿真研究与应用[J].飞行力学,2004,22(1):52-55.
作者姓名:任宏光  周桢
作者单位:1. 北京航空航天大学,工程系统工程系,北京,100083;中国空空导弹研究院,河南,洛阳,471009
2. 中国空空导弹研究院,河南,洛阳,471009
摘    要:针对某新型导弹系统.在六自由度弹道仿真的详细数学模型基础上对各分系统进行合理有效地简化,采用各简化模型以及适当的积分方法和积分步长,对整个导弹快速仿真系统进行实现。在进行精度分析时,将快速仿真系统计算出的导弹允许攻击区与详细仿真的结果进行了对比,对比结果表明:快速仿真得到的发射包线与详细仿真的结果基本一致,满足机载计算机的实时性和快速性要求。

关 键 词:复合制导  空对空导弹  快速仿真  导弹允许攻击区
文章编号:1002-0853(2004)01-0052-04
修稿时间:2003年6月19日

Research and Application of on Quick Simulation for the AAM with Complex Guidance
REN Hong-guang.Research and Application of on Quick Simulation for the AAM with Complex Guidance[J].Flight Dynamics,2004,22(1):52-55.
Authors:REN Hong-guang
Institution:REN Hong-guang~
Abstract:According to the system of a new type missile,we have made further study of the six dimensions detailed simulation model and all subsystems are simplified effectually and in reason.The whole missile's quick-emulation system was realized by the program which is based on the simple models,appropriate integral methods and integral steps. While analyzing the accuracy of the quick simulation, we compare the envelope of the quick simulation with that of detailed simulation.Here is the comparing result-the answer of quick simulation is consistent with that of detailed simulation and can get the result so quickly that it can fit the computer of the fighter better.
Keywords:AAM  quick simulation  complex guidance  missile envelope
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