A new method of determining the satellite initial orbit with attitude data is presented.
提出了一种利用姿态测量数据确定卫星初始轨道的新方法。
This paper introduces methods of calculation the initial orbit of the satellite only with the velocity vectors of two epochs.
本文介绍了仅用卫星两个时刻速度向量计算卫星初轨的方法。
This paper introduces methods of calculation the initial orbit of the satellite only with the velocity vectors of two epochs.
本文介绍了仅用卫星两个时刻速度向量计算卫星初轨的方法。
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