摘要
研究了典型助推器发动机尾焰的红外辐射和传输特性,分析了天基红外系统的探测能力。针对典型的助推飞行模式建立了轨迹跟踪与预估模型,给出了天基红外系统的跟踪与预估能力分析结果。
The infrared radiation of typical rocket exhaust plumes and its characteristics are studied and the detection capability of the Space-Based Infrared System（SBIRS） is analyzed.According to the typical booster flight mode,a trajectory tracking and estimating model is established.The simulation result about the tracking and estimating capability of SBIRS is given.
出处
《红外》
CAS
2016年第6期13-18,共6页
Infrared
关键词
红外
天基探测
跟踪
infrared
space-based detection
tracking
