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首页> 外文期刊>Journal of Spacecraft and Rockets >Orbit Determination and Prediction of the International Space Station
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Orbit Determination and Prediction of the International Space Station

机译:国际空间站的轨道确定和预测

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摘要

The International Space Station is equipped with Global Positioning System receivers that provide real-time position information at the 10 m accuracy level. In preparation of the Atomic Clock Ensemble in Space experiment, measurements from Russian and American receivers have been used to assess the navigation accuracy that can be achieved through postprocessing of navigation solutions and raw data in a precise orbit determination process. In addition, the capability to accurately forecast the space station orbit for operation of microwave and laser terminals has been studied. It is shown that the orbit can be reconstructed with a 1m position accuracy and a 1 mm/s velocity accuracy even from single-frequency Global Positioning System measurements. For the test period in mid 2006, short arc orbit predictions with a median error of 20 and 70 m could be obtained over forecast intervals of 6 and 12 h, respectively. The navigation accuracy obtained is compatible with the mission requirements for the relativistic correction of the atomic clocks and the quick look clock performance monitoring.
机译:国际空间站配备了全球定位系统接收器,可提供10 m精度级别的实时位置信息。在准备太空原子钟组实验时,已使用来自俄罗斯和美国接收器的测量值来评估导航精度,该精度可通过在精确的轨道确定过程中对导航解决方案和原始数据进行后处理来实现。此外,还研究了准确预测空间站轨道以运行微波和激光终端的能力。结果表明,即使通过单频全球定位系统测量,也可以以1m的位置精度和1 mm / s的速度精度重建轨道。在2006年中期的测试期间,可以分别在6和12 h的预测间隔内获得中值误差为20和70 m的短弧轨道预测。获得的导航精度与原子钟的相对论校正和快速查看时钟性能监控的任务要求兼容。

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