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Next: Osculating Orbital Elements Up: Orbital Perturbation Theory Previous: Introduction

Disturbing Function

For the moment, let us consider a simplified Solar System that consists of the Sun and two planets--see Figure 33. Let the Sun be of mass $M$, and position vector ${\bf R}_s$. Likewise, let the two planets have masses $m$ and $m'$, and position vectors ${\bf R}$ and ${\bf R}'$, respectively. Here, we are assuming that $m,\,m'\ll M$. Let ${\bf r} = {\bf R}-{\bf R}_s$ and ${\bf r}'={\bf R}'-{\bf R}_s$, be the position vector of each planet relative to the Sun. Without loss of generality, we can assume that $r'>r$.

Figure 33: A simplified model of the Solar System.
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Now, the equations of motion of the various elements of our simplified Solar System are

$\displaystyle M\,\ddot{\bf R}_s$ $\textstyle =$ $\displaystyle G\,M\,m\,\frac{\bf r}{r^{\,3}} + G\,M\,m'\,\frac{{\bf r}'}{r'^{\,3}},$ (730)
$\displaystyle m\,\ddot{\bf R}$ $\textstyle =$ $\displaystyle G\,m\,m'\,\frac{{\bf r}'-{\bf r}}{\vert{\bf r}'-{\bf r}\vert^{\,3}}
- G\,m\,M\,\frac{{\bf r}}{r^{\,3}},$ (731)
$\displaystyle m'\,\ddot{\bf R}'$ $\textstyle =$ $\displaystyle G\,m'\,m\,\frac{{\bf r}-{\bf r}'}{\vert{\bf r}-{\bf r}'\vert^{\,3}}
- G\,m'\,M\,\frac{{\bf r}'}{r'^{\,3}},$ (732)

It thus follows that
$\displaystyle \ddot{\bf r} + \mu\,\frac{\bf r}{r^{\,3}}$ $\textstyle =$ $\displaystyle G\,m'\left(\frac{{\bf r}'-{\bf r}}{\vert{\bf r}'-{\bf r}\vert^{\,3}} - \frac{{\bf r}'}{r'^{\,3}}\right),$ (733)
$\displaystyle \ddot{\bf r}' + \mu'\,\frac{{\bf r}'}{r'^{\,3}}$ $\textstyle =$ $\displaystyle G\,m\left(\frac{{\bf r}-{\bf r}'}{\vert{\bf r}-{\bf r}'\vert^{\,3}} - \frac{{\bf r}}{r^{\,3}}\right),$ (734)

where $\mu= G\,(M+m)$, and $\mu'=G\,(M+m')$. The right-hand sides of the above equations specify the interplanetary interaction forces that were neglected in our previous analysis. These right-hand sides can be conveniently expressed as the gradients of potentials: i.e.,
$\displaystyle \ddot{\bf r} + \mu\,\frac{\bf r}{r^{\,3}}$ $\textstyle =$ $\displaystyle \nabla {\cal R},$ (735)
$\displaystyle \ddot{\bf r}' + \mu'\,\frac{{\bf r}'}{r'^{\,3}}$ $\textstyle =$ $\displaystyle \nabla' {\cal R}',$ (736)

where
$\displaystyle {\cal R}({\bf r},{\bf r}')$ $\textstyle =$ $\displaystyle \tilde{\mu}'\left(\frac{1}{\vert{\bf r}-{\bf r}'\vert} - \frac{{\bf r}\cdot{\bf r}'}{r'^{\,3}}\right),$ (737)
$\displaystyle {\cal R}' ({\bf r},{\bf r}')$ $\textstyle =$ $\displaystyle \tilde{\mu}\left(\frac{1}{\vert{\bf r}-{\bf r}'\vert} - \frac{{\bf r}\cdot{\bf r}'}{r^{\,3}}\right),$ (738)

with $\tilde{\mu} = G\,m$, and $\tilde{\mu}'=G\,m'$. Here, ${\cal R}({\bf r},{\bf r}')$ and ${\cal R}'({\bf r}, {\bf r}')$ are termed disturbing functions. Moreover, $\nabla$ and $\nabla'$ are the gradient operators involving the unprimed and primed coordinates, respectively.


next up previous
Next: Osculating Orbital Elements Up: Orbital Perturbation Theory Previous: Introduction
Richard Fitzpatrick 2011-04-22