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Attitude determination of Galileo satellites using high-resolution kHz SLR

机译:使用高分辨率kHz SLR确定伽利略卫星的姿态

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A Galileo retroreflector panel was mounted on a tripod 32 km outside of the satellite laser ranging station Graz. The panel was tilted to achieve laser beam incident angles between 0 circledocumentclass[12pt]{minimal} usepackage{amsmath} usepackage{wasysym} usepackage{amsfonts} usepackage{amssymb} usepackage{amsbsy} usepackage{mathrsfs} usepackage{upgreek} setlength{oddsidemargin}{-69pt} egin{document}$$0<^>{circ }$$end{document} and approx. 18 circledocumentclass[12pt]{minimal} usepackage{amsmath} usepackage{wasysym} usepackage{amsfonts} usepackage{amssymb} usepackage{amsbsy} usepackage{mathrsfs} usepackage{upgreek} setlength{oddsidemargin}{-69pt} egin{document}$$18<^>{circ }$$end{document} while simultaneously doing distance measurements. At incident angles larger than approx. 8 circledocumentclass[12pt]{minimal} usepackage{amsmath} usepackage{wasysym} usepackage{amsfonts} usepackage{amssymb} usepackage{amsbsy} usepackage{mathrsfs} usepackage{upgreek} setlength{oddsidemargin}{-69pt} egin{document}$$8<^>{circ }$$end{document} it was possible to identify fine structures within the data corresponding to the different columns of retroreflectors within the panel. The range differences between these columns were determined via a histogram analysis. Knowing the panel geometry it was possible to recalculate the laser beam incident angle on the panel. To compare these ground-based measurements to measurements to a specific pass of Galileo 103, matching incident angle conditions were chosen. Similar structures were found within the data set and it was possible to verify the incident angle of the laser beam. Such a method provides an excellent way to validate the attitude of Galileo satellites and is possible by analyzing the fine details of mm-accuracy kHz SLR data only.
机译:Galileo后向反射器面板安装在卫星激光测距站Graz外32公里处的三脚架上。倾斜面板使激光束的入射角达到0圆 documentclass [12pt] {最小} usepackage {amsmath} usepackage {wasysym} usepackage {amsfonts} usepackage {amssymb} usepackage {amsbsy} usepackage {mathrsfs } usepackage {upgreek} setlength { oddsidemargin} {-69pt} begin {document} $$ 0 <^> { circ} $$ end {document}左右。 18 circle documentclass [12pt] {minimum} usepackage {amsmath} usepackage {wasysym} usepackage {amsfonts} usepackage {amssymb} usepackage {amsbsy} usepackage {mathrsfs} usepackage {upgreek} setlength { oddsidemargin } {-69pt} begin {document} $$ 18 <^> { circ} $$ end {document},同时进行距离测量。入射角大于约8 circle documentclass [12pt] {minimum} usepackage {amsmath} usepackage {wasysym} usepackage {amsfonts} usepackage {amssymb} usepackage {amsbsy} usepackage {mathrsfs} usepackage {upgreek} setlength { oddsidemargin } {-69pt} begin {document} $$ 8 <^> { circ} $$ end {document},可以识别数据中与面板内后向反射器不同列相对应的精细结构。这些列之间的范围差异是通过直方图分析确定的。了解了面板的几何形状,便可以重新计算面板上的激光束入射角。为了将这些基于地面的测量结果与对Galileo 103特定行程的测量结果进行比较,选择了匹配的入射角条件。在数据集中发现了类似的结构,可以验证激光束的入射角。这种方法提供了一种验证伽利略卫星姿态的极好方法,并且仅通过分析毫米精度kHz SLR数据的精细细节就可以实现。

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