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针对国外新一代高速导弹的特点,结合红外成像探测系统要求及其工作环境,开展凝视红外成像探测系统在高速导弹上应用的性能测试和评估方法研究,提出了高速导弹气动光学效应环境的分析与测试方法和气动光学效应下的末制导探测系统性能测试评估方法,并通过风洞试验、数学仿真和实验室性能测试试验进行红外成像末制导系统各项性能的测试,从而全面评估红外成像末制导系统在高速导弹中的应用性能,为开展凝视红外成像末制导系统的设计和优化提供了重要依据和指导。
Aiming at the characteristics of a new generation of high-speed missiles in foreign countries, combined with the requirements of infrared imaging detection system and its working environment, the research on the performance testing and evaluation methods of gaze infrared imaging detection system on high-speed missiles is put forward. The analysis and application of high-speed missile aerodynamic optical environment Test method and aerodynamic optical effect of the end-guidance detection system performance testing and evaluation methods and wind tunnel test, mathematical simulation and laboratory performance testing of infrared imaging terminal guidance system performance testing, so as to fully assess the end of the infrared imaging guidance The application performance of the system in high-speed missile provides an important basis and guidance for the design and optimization of the end-guidance system of gaze infrared imaging.