It is convenient to evaluate the disturbing function,
![$\displaystyle {\cal R}({\bf r},{\bf r}')= \mu'\left(\frac{1}{\vert{\bf r}-{\bf r}'\vert} - \frac{{\bf r}\cdot{\bf r}'}{r'^{\,3}}\right),$](img4137.png) |
(B.23) |
in a frame of reference that is instantaneously aligned with the ecliptic plane, as described in Section 4.12.
Let (
,
,
) and (
,
,
) be the Cartesian components of
and
, respectively, in this
standard reference frame. It follows from Equations (4.38), and (4.72)–(4.74), that
as well as
where
Here,
,
,
,
,
, and
are the orbital true anomaly, major radius, eccentricity, inclination, argument of the perihelion, and
longitude of the ascending node, respectively, of Mercury. Moreover,
,
,
,
,
, and
are the
corresponding quantities for the perturbing planet.
It is helpful to define
Making use of Equations (B.25)–(B.30), we deduce that
and
Hence,
![$\displaystyle {\cal R}(r,\theta) = \mu'\left[\frac{1}{(r^{\,2} + r'^{\,2}-2\,r\,r'\,\beta)^{1/2}}-\frac{\beta\,r}{r'^{\,2}}\right],$](img4188.png) |
(B.36) |
which implies that
![$\displaystyle \frac{\partial{\cal R}}{\partial r} =- \mu'\,r'\left[\frac{r/r'-\beta}{(r^{\,2} + r'^{\,2}-2\,r\,r'\,\beta)^{3/2}} + \frac{\beta}{r'^{\,3}}\right],$](img4189.png) |
(B.37) |
and
![$\displaystyle \frac{1}{r}\,\frac{\partial{\cal R}}{\partial\theta} = \mu'\,r'\,...
...rac{1}{(r^{\,2} + r'^{\,2}-2\,r\,r'\,\beta)^{3/2}} - \frac{1}{r'^{\,3}}\right],$](img4190.png) |
(B.38) |