Kepler equation solution without transcendental functions or lookup tables

Adonis R. Pimienta-Penalver, John L. Crassidis
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Abstract

This paper presents a new approach to approximate the solution of Kepler’s equation. It is found that by means of a series approximation, an angle identity, the application of Sturm’s theorem, and an iterative correction method, the need to evaluate transcendental functions or query lookup tables is eliminated. The final procedure builds upon Mikkola’s approach. Initially, a fifteenth-order polynomial is derived through a series approximation of Kepler’s equation. Sturm’s theorem is used to prove that only one real root exists for this polynomial for the given range of mean anomaly and eccentricity. An initial approximation for this root is found using a third-order polynomial. Then, a single generalized Newton–Raphson correction is applied to obtain fourteenth-place accuracies in the elliptical case, which is near machine precision. This paper will focus on demonstrating the procedure for the elliptical case, though an application to hyperbolic orbits through a similar methodology may be similarly developed.

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无需超越函数或查找表的开普勒方程解法
本文提出了一种近似求解开普勒方程的新方法。研究发现,通过数列近似、角度特性、斯特姆定理的应用以及迭代修正法,无需对超越函数进行求值或查询查找表。最后的程序以 Mikkola 的方法为基础。首先,通过对开普勒方程进行串联逼近,得出十五阶多项式。斯特姆定理被用来证明,在给定的平均异常和偏心率范围内,这个多项式只存在一个实数根。利用三阶多项式找到了这个根的初始近似值。然后,应用单一的广义牛顿-拉夫逊修正法在椭圆情况下获得 14 位精度,接近机器精度。本文将重点演示椭圆情况下的程序,不过也可以通过类似的方法应用于双曲线轨道。
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