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An Advanced Analysis Method of Initial Orbit Determination with Too Short Arc Data

机译:具有太短电弧数据的初始轨道确定的高级分析方法

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This paper studies the initial orbit determination (IOD) based on space-based angle measurement. Commonly, these space-based observations have short durations. As a result, classical initial orbit determination algorithms give poor results, such as Laplace methods and Gauss methods. In this paper, an advanced analysis method of initial orbit determination is developed for space-based observations. The admissible region and triangulation are introduced in the method. Genetic algorithm is also used for adding some constraints of parameters. Simulation results show that the algorithm can successfully complete the initial orbit determination.
机译:本文研究了基于空间的角度测量的初始轨道测定(IOD)。通常,这些基于空间的观测有短持续时间。结果,经典初始轨道确定算法产生较差的结果,例如拉普拉斯方法和高斯方法。本文开发了一种高级分析方法,用于基于空间的观察。可允许的区域和三角测量在该方法中引入。遗传算法还用于添加一些参数约束。仿真结果表明,该算法可以成功完成初始轨道确定。

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