临近空间基目标探测仿真实验设计

Simulation Experiment Design for Target Detection Based on Near Space Platform

  • 摘要: 临近空间基探测能增大探测距离,能有效解决对隐身飞机、临近空间飞行器、预警机的探测。为方便实验教学,该文以临近空间基探测预警机为例,介绍了该仿真实验设计的过程。分别针对地基探测、空基探测和临近空间基探测预警机,计算了红外大气透过率,研究了临近空间基红外探测预警机的有效性。以预警机尾喷管及尾焰为主要辐射源,采用分离隐式分解,从多角度分层计算了预警机尾焰在临近空间的红外辐射特性。在临近空间基不同探测方位角下,计算了对预警机的红外探测距离。该仿真可应用于实验教学,也为临近空间基红外探测预警机提供了参考价值。

     

    Abstract: The target detection based on near space platform can increase the detection distance, which can effectively solve the detection problem for stealth aircraft, near space vehicle and early warming aircraft (EWA).To facilitate experiment education, this paper provides the simulation experiment design process with the example of detecting EWA based on near space platform.Infrared atmospheric transmittance are derived for detecting EWA from ground-base, air-based and near space-based loctions, respectively, and the effectiveness of EWA based on infrared detection from near space is investigated.The nozzle and exhaust plume of EWA are considered as the main source of radiation and the characteristics of exhaust plume‘s infrared radiation in near space is derived in multiple azimuths using separated implicit decomposition.The infrared detecting distance of the EWA is derived from near space under different azimuths.This study can be applied to the experiment teaching, and it also provides a reference for infrared detection of EWA based on near space platform.

     

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