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作 者:李迎博 谭黎立 梁卓[1] 胡骁 LI Ying-bo;TAN Li-li;LIANG Zhuo;HU Xiao(China Academy of Launch Vehicle Technology,Beijing 100076,China)
出 处:《计算机仿真》2023年第9期13-17,48,共6页Computer Simulation
摘 要:战术导弹和作战飞机的高速发展,给防空导弹提出了更高的要求。导弹的制导系统担负着目标探测、飞行导引等重要任务,是整个武器系统的关键组成部分。对制导系统进行性能评估,一方面可以评估制导算法的优劣,从而确定最适合导弹的制导方案;另一方面,评估结果可以作为重要子指标,供后续武器系统性能评估使用。以爱国者-3防空导弹为研究对象,建立起其制导系统性能评估指标体系,并使用一种灰色系统理论与层次分析法相结合的方法对制导系统进行性能评估。通过实际评估结果,证明了指标体系和评估方法的合理性。The rapid development of tactical missiles and combat aircraft puts forward higher requirements for air defense missiles.The missile guidance system undertakes the important tasks of target detection and flight guidance,and is the key component of the whole weapon system.On the one hand,the performance evaluation of the guidance system can evaluate the advantages and disadvantages of the guidance algorithm,so as to determine the most suitable guidance scheme for the missile.On the other hand,the evaluation results can be used as important sub-indicators for subsequent weapon system performance evaluation.Taking the PAC-3 defense missile as the research object,the evaluation index system of the missile guidance system is established,and a method combining grey theory and analytic hierarchy process is used to evaluate the performance of the guidance system.Through the actual evaluation results,the rationality of the index system and evaluation system is proved.
分 类 号:TP391.9[自动化与计算机技术—计算机应用技术]
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