宇航学报
宇航學報
우항학보
JOURNAL OF ASTRONAUTICS
2010年
2期
489-494
,共6页
SAR%平台定位%最小二乘支持向量机%曲线拟合%误差传递
SAR%平檯定位%最小二乘支持嚮量機%麯線擬閤%誤差傳遞
SAR%평태정위%최소이승지지향량궤%곡선의합%오차전체
SAR%Platform geo-location%LSSVM%Curve fitting%Error propagation
将SAR平台定位分解为粗略定位和精确定位两个阶段.首先,在SAR正侧视成像的条件下,利用某个方位门内的所有控制点,采用非线性最小二乘平差粗略估计出SAR平台在该方位时刻的空间位置,并从理论上推导了控制点的误差协方差矩阵到SAR平台定位的误差协方差矩阵的传递规律.其次,利用各个方位时刻粗略估计的SAR平台位置,采用最小二乘支持向量回归机精确估计SAR平台的运动方程,从而精确估计SAR平台在某个时刻的空间位置.仿真试验表明,本文提出的方法能够精确地反演出SAR平台的空间位置.
將SAR平檯定位分解為粗略定位和精確定位兩箇階段.首先,在SAR正側視成像的條件下,利用某箇方位門內的所有控製點,採用非線性最小二乘平差粗略估計齣SAR平檯在該方位時刻的空間位置,併從理論上推導瞭控製點的誤差協方差矩陣到SAR平檯定位的誤差協方差矩陣的傳遞規律.其次,利用各箇方位時刻粗略估計的SAR平檯位置,採用最小二乘支持嚮量迴歸機精確估計SAR平檯的運動方程,從而精確估計SAR平檯在某箇時刻的空間位置.倣真試驗錶明,本文提齣的方法能夠精確地反縯齣SAR平檯的空間位置.
장SAR평태정위분해위조략정위화정학정위량개계단.수선,재SAR정측시성상적조건하,이용모개방위문내적소유공제점,채용비선성최소이승평차조략고계출SAR평태재해방위시각적공간위치,병종이론상추도료공제점적오차협방차구진도SAR평태정위적오차협방차구진적전체규률.기차,이용각개방위시각조략고계적SAR평태위치,채용최소이승지지향량회귀궤정학고계SAR평태적운동방정,종이정학고계SAR평태재모개시각적공간위치.방진시험표명,본문제출적방법능구정학지반연출SAR평태적공간위치.
The SAR geo-location method is composed of two stages. The first stage employs a nonlinear least squares adjustment method which using all control points in an azimuth door to coarsely estimate the SAR platform location at the azimuth time under zero imaging squint angle. And the error propagation law from control point to coarse SAR position is deduced theoretically. The second stage employs a least squares support vector machine which based on coarsely evaluated SAR positions at each azimuth time to finely estimate the SAR platform motion equation in the imaging process. And the accurate SAR platform position at any time is calculated by the least squares support vector machine. Simulated experiment results show the excellent performance of the SAR geo-location method proposed in this paper.