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arXiv 2111.02406astro-ph.EPmath-phmath.MP
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用开普勒积分定轨

Orbit determination with the Keplerian integrals

Giovanni Federico Gronchi

摘要:

本文综述了两种适用于太阳系天体光学观测的过短弧初轨确定方法。这些方法采用开普勒问题的守恒定律,并允许尝试联系TSAs,这些TSAs指的是相当远的时期,甚至比观测对象的轨道周期多一个。第一种方法({\tt Link2})涉及2个TSA的连接,并且导致9次的单变量多项式方程。利用Gröbner基理论证明了该多项式的一个最优性质。第二种方法({\tt Link3})被认为是用于3个TSA的链接,并且导致8次的单变量多项式方程。这两种算法的数值试验。

英文摘要:

We review two initial orbit determination methods for too short arcs (TSAs) of optical observations of a solar system body. These methods employ the conservation laws of Kepler's problem, and allow to attempt the linkage of TSAs referring to quite far epochs, differing by even more than one orbital period of the observed object. The first method ({\tt Link2}) concerns the linkage of 2 TSAs, and leads to a univariate polynomial equation of degree 9. An optimal property of this polynomial is proved using Gröbner bases theory. The second method ({\tt Link3}) is thought for the linkage of 3 TSAs, and leads to a univariate polynomial equation of degree 8. A numerical test is shown for both algorithms.

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