It is convenient to evaluate the disturbing function,
|
(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,
|
(B.36) |
which implies that
|
(B.37) |
and
|
(B.38) |