摘要
针对大椭圆轨道合成孔径雷达存在大偏心率,时变轨道高度及时变卫星速度等特性,首次开展了大椭圆轨道SAR滑动模式设计研究.对大椭圆轨道SAR滑动聚束模式设计,考虑了不同轨道位置处不同分辨率改善因子、地面波束足迹一致性、天线扫描角度、天线扫描角速度等.对大椭圆轨道SAR滑动聚束模式回波斜距模型研究.仿真分析结果表明大椭圆轨道SAR滑动聚束模式参数需要随轨道位置变化进行调整,为了满足成像需求斜距模型需要展开到三阶.
Focusing on the characteristics of large eccentricity,time-varying orbit height and satellite speed in elliptical orbit SAR,the sliding mode design was studied for large elliptical orbit SAR.Firstly,considering different resolution improvement factors at different orbital positions,ground beam footprint consistency,antenna scanning angle,antenna scanning angular velocity and so on,a sliding spotlight mode was designed for large elliptical orbit SAR.Then,the slant range model of gliding spotlight mode echo was studied.Finally,a simulation validation was carried out.The simulation results show that the parameters of sliding spotlight mode for elliptical orbit SAR need to be adjusted with the change of orbit position.In order to meet the imaging requirements,the slant model needs to be expanded to third order.
作者
李立
李财品
何明一
LI Li;LI Cai-pin;HE Ming-yi(School of Electrical and Information,Northwestern Polytechnic University,Xi’an,Shannxi 710129,China;China Academy of Space Technology,Xi’an,Shannxi 710072,China)
出处
《北京理工大学学报》
EI
CAS
CSCD
北大核心
2020年第5期552-561,共10页
Transactions of Beijing Institute of Technology
基金
国家部委基金资助项目(61404130307,61400030302)。
