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Remote sensing polar orbiting satellites tracking using orbital elements

机译:使用轨道元素遥感极性轨道卫星跟踪

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Main parameters to track a remote sensing polar orbiting satellite are satellite's rising time, setting time, overhead time, visibility duration and maximum elevation angle indicating the closeness of the satellite path above the station. Since direct calculation of the parameters is complicated and time consuming, a look up table for satellite tracking is constructed in this study. This solution provides fast access to the required tracking parameters in addition to overcoming the problem of direct calculation of required parameters. The look up table construction is performed in two stages. In the first stage, orbital elements are used to determine the satellite position using a keplerian orbit model. At this stage, the visibility duration is divided into small equally spaced time intervals. Then, satellite position is determined using orbital elements at the start of any time interval within the visibility duration. The second stage is involved with the calculation of pointing parameters from the ground station antenna to the satellite position. The look up table which contains zenith and azimuth angles as pointing parameters versus time is used directly by the receiving antenna servo motors to track the satellite. The proposed polar orbiting satellite tracking procedure has been successfully tested on NOAA satellite for AVHRR data acquisition. The proposed algorithm based on its simplicity has shown sufficient accuracy at much higher implementation speed compared with other methods.
机译:主要参数来跟踪遥感极地轨道卫星是卫星的上升时间,凝结时间,开销时间,可见持续时间和最大仰角指示站上方的卫星路径的接近程度。由于参数的直接计算是复杂和耗时的,一看表卫星跟踪本研究构建。该解决方案提供了除了克服所需的参数直接计算的问题快速访问到所需的跟踪参数。查找表建设分两个阶段进行。在第一阶段中,轨道参数被用于确定用开普勒轨道模型中的卫星位置。在此阶段,可见持续时间被划分成小的等间隔的时间间隔。然后,卫星位置是使用轨道元件的可见持续时间内的任何时间间隔的开始来确定。第二阶段涉及从地面站天线到卫星位置指向参数的计算。查找表含有天顶角和方位角为指向参数对时间的直接使用的接收天线的伺服电机来跟踪卫星。拟议的极地轨道卫星跟踪程序对NOAA卫星AVHRR用于数据采集试验成功。基于其简单性,该算法与其他方法相比表现出足够的精度高得多的执行速度。

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