Evolution equations for two-planet solar system
For the moment, let us consider a simplified solar system that consists
of the Sun and two planets. See Figure 10.1. Let the Sun be of mass and position
vector . Likewise, let the two planets have masses and
and position vectors and , respectively. Here, we are
assuming that
. Finally, let
and
be the position vector of each planet
relative to the Sun. Without loss of generality, we can assume that .
Figure 10.1:
A simplified model of the solar system.
|
In an inertial reference frame, the equations of motion of the various elements of our simplified
solar system are
It thus follows that
where
and
. The right-hand
sides of these 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:
where
with
, and
. Here,
and
are termed disturbing functions. Moreover, and are the gradient operators involving the
unprimed and primed coordinates, respectively.
In the absence of the second planet, the orbit of the first planet is fully described by its
six standard orbital elements (which are constants of its motion): the major radius, ; the mean longitude at epoch,
; the eccentricity, ;
the inclination (to the ecliptic plane), ; the longitude of the perihelion,
; and the longitude of the ascending node,
. (See Section 4.12.) As described in Appendix G, the perturbing influence of the second planet
causes these elements to slowly evolve in time. Such time-varying orbital elements are generally known as osculating
elements.10.1
Actually, when describing the aforementioned evolution, it is more convenient to
work in terms of an alternative set of osculating elements, namely,
,
,
,
,
, and
. Here,
and
, where
is the unperturbed mean
orbital angular velocity. In the following, for ease of notation, and are written simply as and , respectively. Furthermore,
will be used as shorthand for
.
The evolution equations for the first planet's osculating orbital elements
take the form (see Section H.2)
where (see Section H.3)
Here,
,
, and
|
(10.19) |
where ,
, , , , are the osculating orbital elements of the second planet.
The factors are known as Laplace coefficients (Brouwer and Clemence 1961).
In deriving these expressions from Equations (10.6) and (10.8), we have expanded to first order in the ratio of the planetary masses to the
solar mass; we have then evaluated the secular terms in the disturbing
functions (i.e., the terms that are independent of
and
) to second order in the orbital eccentricities and inclinations. The nonsecular terms in the disturbing functions are
evaluated to first order in the
eccentricities and inclinations. (See Appendix H.) This expansion procedure is reasonable because the planets all have very small masses compared with that of the
Sun, and also have relatively small orbital eccentricities and inclinations.
There is an analogous set of equations, which can be derived from Equations (10.7) and (10.9), that describe the time evolution of the osculating orbital elements
of the second planet due to the perturbing influence of the first. These take the form (see Section H.2)
where (see Section H.3)
Here,
, and
.