Displacement Norm in the Presence of an Inverse-Square Perturbing Acceleration in the Reference Frame Associated with the Velocity Vector

IF 0.7 4区 物理与天体物理 Q3 ASTRONOMY & ASTROPHYSICS
T. N. Sannikova
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引用次数: 0

Abstract

The problem of motion of a zero-mass-point under the action of attraction to the central body and a small perturbing acceleration \({\mathbf{P}}{\kern 1pt} ' = {\mathbf{P}}{\text{/}}{{r}^{2}}\) is considered, where \(r\) is the distance to the attracting center and components of the vector \({\mathbf{P}}\) are assumed to be constant in a reference system with the axes directed along the velocity vector, the main normal, and the angular momentum vector. Previously, for this problem, equations of motion in the mean elements and formulas for the transition from osculating elements to the mean ones in the first order of smallness were found; second-order quantities are neglected. If the perturbing forces are small, then the osculating orbit slightly deviates from the mean one. The difference \(d{\mathbf{r}}\) between the position vectors on the osculating and mean orbit is a quasi-periodic function of time. In this work, the Euclidean (root-mean-square over the mean anomaly) norm \({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\) of the displacement of the osculating orbit relative to the mean one is obtained. It turned out that \({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\) depends only on the components of the vector \({\mathbf{P}}\) (positive definite quadratic form), the semi-major axis (proportional to the second power), and the eccentricity of the osculating ellipse. The norm \({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\) is obtained in the form of a series in powers of eccentricity \(e\). The resulting expression holds up to \({{e}_{0}} \approx 0.995862\); for \(e > {{e}_{0}}\), \(\varrho = \sqrt {{{{\left\| {d{\mathbf{r}}} \right\|}}^{2}}} \) can take complex values. The results are applied to the problem of the motion of model bodies under the action of perturbing acceleration caused by the Yarkovsky effect. A comparison of the results with similar ones for the norm \({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\) in the reference system associated with the radius vector was also carried out.

Abstract Image

速度矢量参照系中存在反平方扰动加速度时的位移范数
考虑了零质量点在对中心物体的吸引力和一个小的扰动加速度\({\mathbf{P}}{\kern 1pt} ' = {\mathbf{P}}{\text{/}}{{r}^{2}}\)的作用下的运动问题,其中\(r\)是到吸引中心的距离,并且假设矢量\({\mathbf{P}}\)的分量在一个轴沿速度矢量、主法线矢量和角动量矢量方向的参照系中是恒定的。在此之前,对于该问题,已经找到了平均单元的运动方程和从密切单元到平均单元的一阶小位移的过渡公式;二阶量被忽略了。如果摄动力很小,则闭合轨道与平均轨道有轻微偏差。在密切轨道和平均轨道上的位置向量的差\(d{\mathbf{r}}\)是时间的准周期函数。在这项工作中,获得了相对于平均轨道位移的欧几里得(均方根异常)范数\({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\)。原来\({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\)只取决于矢量\({\mathbf{P}}\)(正定二次型)、半长轴(与二次幂成正比)和密切椭圆的偏心率的分量。范数\({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\)以一系列偏心率幂\(e\)的形式得到。结果表达式支持\({{e}_{0}} \approx 0.995862\);对于\(e > {{e}_{0}}\), \(\varrho = \sqrt {{{{\left\| {d{\mathbf{r}}} \right\|}}^{2}}} \)可以取复数值。将所得结果应用于亚尔科夫斯基效应引起的扰动加速度作用下模型体的运动问题。将结果与参考系统中与半径矢量相关的规范\({{\left\| {d{\mathbf{r}}} \right\|}^{2}}\)的类似结果进行了比较。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Astronomy Reports
Astronomy Reports 地学天文-天文与天体物理
CiteScore
1.40
自引率
20.00%
发文量
57
审稿时长
6-12 weeks
期刊介绍: Astronomy Reports is an international peer reviewed journal that publishes original papers on astronomical topics, including theoretical and observational astrophysics, physics of the Sun, planetary astrophysics, radio astronomy, stellar astronomy, celestial mechanics, and astronomy methods and instrumentation.
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