Perturbed Robe’s Restricted Problem of 2+2 Bodies when the primaries form a Roche Ellipsoid - Triaxial System
Bhavneet Kaur1, Rajiv Aggarwal2, Sushil Yadav3
1Lady Shri Ram College for Women, Delhi University, Delhi, India
2Shri Aurobindo College, Delhi University, Delhi, India
3Maharaja Agrasen College, Delhi University, Delhi, India
*Corresponding Author Email: bhavneet.lsr@gmail.com, rajiv_agg1973@yahoo.com, sushilyadav1973@rediffmail.com
ABSTRACT:
The aim of this paper is to study the effect of
perturbations in the Coriolis and centrifugal forces on the location and
stability of the equilibrium solutions in the Robe’s restricted problem of 2+2
bodies under the assumption that the hydrostatic equilibrium figure of the
first primary is a Roche ellipsoid and the shape of the second primary is
triaxial.The third and the fourth bodies (of mass
and
respectively)
are small solid spheres of density
and
respectively
inside the ellipsoid, with the assumption that the mass and the radius of the
third and the fourth body are infinitesimal. We assume that
is describing a
circle around
. The masses
and
mutually
attract each other, do not influence the motion of
and
but are influenced
by them. We have taken into consideration all the three components of the
pressure field in deriving the expression for the buoyancy force viz (i) due to
the own gravitational field of the fluid (ii)that originating in the attraction
of
(iii) that
arising from the centrifugal force. The linear stability of this configuration
is examined. It is observed that there exist only six equilibrium solutions of
the system, provided they lie within the Roche ellipsoid. The equilibrium
solutions of
and
lying on
-axis are
unstable for
and
and stable for
and
, using the data
of submarines in the Earth -Moon system. The equilibrium solutions of
and
respectively
when the displacement is given in the direction of
or
axis are
conditionally stable.We observe that the conditions of stability are influenced
by the small perturbations in the Coriolis and centrifugal forces.
KEYWORDS: Robe’s Restricted Problem; Roche Ellipsoid; Triaxial; Stability.
Robe (1977) has investigated
a new kind of restricted three-body problem in which one of the primaries of
mass
is a rigid spherical shell filled with a homogeneous
incompressible fluid of density
. The smaller primary is a mass point
outside the shell. The third body of mass
, supposed moving inside the shell, is a small solid
sphere of density
, with the assumption that the mass and the radius of
the third body are infinitesimal. He assumed that the mass
describes a Keplerian orbit around the mass
. He has proved that the centre of the first primary,
is the only equilibrium solution for all values of the density parameter
, mass parameter
, eccentricity parameter
. Further, he has discussed the linear stability of
this equilibrium solution. He has explicitly discussed two cases. In the first
case, the orbit of
around
is circular and in the second case, the orbit is
elliptic, but the shell is empty (i.e. no fluid inside it) or the densities of
and
are equal. In each case, the domain of stability has
been investigated for the whole range of parameters occurring in the problem.
In the above problem, the
existence of only one equilibrium solution namely, centre of the first primary
is discussed. Hallan & Rana(2001) studied the existence and the linear
stability of all the equilibrium solutions in the Robe’s restricted three-body
problem. They have proved that besides the centre, there are other equilibrium
solutions too which exist only when the density parameter
and the second primary moves around the first in a
circular orbit.
Szebehely(1967) considered
the effect of small perturbations in the Coriolis force on the stability of
equilibrium points in the classical restricted problem, keeping the centrifugal
force constant and proved that the collinear points remain unstable. The range
of stability of the triangular equilibrium points increase or decrease
depending upon whether the change
in the Coriolis force is positive or negative thereby
establishing that the Coriolis force is a stabilizing force.In the same
problem, Bhatnagar & Hallan(1978) studied the effect of the changes
and
in the Coriolis and centrifugal forces respectively
on the stability of equilibrium points and concluded that the collinear points
remain unstable. For the triangular equilibrium points, the range of stability
increases or decreases depending upon whether the point
lie in one or the other of the two parts in which the
line
divides the
plane.
The Robe’s problem has been
varied by the introduction of perturbing forces by many researchers. Shrivastava
and Garain (1991) examined the effect of small perturbations in the Coriolis
and centrifugal forces on the position of the equilibrium point. In obtaining
position of the equilibrium point, they considered the circular case with equal
densities (i.e.
). While evaluating the buoyancy force, bothRobe
(1977) and Shrivastava and Garain (1991)assumed that the pressure field of the
fluid has spherical symmetry around the centre of the shell and they considered
only one of the three components of the pressure field, which is, that due to
the own gravitational field of the fluid
. The other two components which are those arising
from the centrifugal force and attraction of
were ignored. Plastino & Plastino (1995) took
into account all these components of the pressure field. They assumed the
hydrostatic equilibrium figure of the first primary as a Roche ellipsoid (Chandrashekhar(1987)).
Hallan&Mangang(2007) examined Robe’s circular restricted three-body problem by considering the buoyancy force as done byPlastino&Plastino (1995). They assumed the hydrostatic equilibrium figure of the first primary as an oblate spheroid and considered the full potential due to the second primary. They found conditions for the existence of an infinite number of equilibrium points and analysed their stability.
Singh and Mohammed (2012) studied the Robe’s circular restricted three-body problem under oblate and triaxial primaries. Singh and Sandah (2012) studied the existence and linear stability of equilibrium points in the Robe’s restricted three-body problem with oblateness. Singh and Mohammed (2013) studied the out-of-plane equilibrium points and their stability in the Robe’s problem with oblateness and triaxiality. Hallan&Rana(2003) studied the effect of perturbations in the Coriolis and centrifugal forces on the location and stability of the equilibrium points in the Robe’s circular restricted problem with density parameter having arbitrary value.
Many authors have worked on
problem of 2+2 bodies. Significant work is that of Whipple(1984). He studied
equilibrium solutions of the restricted problem of 2+2 bodies. He further
studied the linear stability of all the equilibrium solutions.Bhavneet & Rajiv(2012)
extended the Robe’s restricted three-body problem to
bodies. Bhavneet & Rajiv(2013) studied the Robe’s
restricted problem of 2+2 bodies when the bigger primary is a Roche ellipsoid.
They studied the equilibrium solutions of the infinitesimal masses and analysed
their linear stability. Bhavneet & Rajiv(2013) studied Robe’s restricted
problem of 2+2 bodies when the bigger primary is a Roche ellipsoid and the
smaller primary is an oblate body. They studied the equilibrium solutions of
the infinitesimal masses and analysed their linear stability.
Our aim in this paper is to study the effect of perturbations in the Coriolis and centrifugal forces on the location and stability of equilibrium points in Robe’s restricted problem of 2+2 bodies considering the effect of the full buoyancy force of the fluid of the first primary and taking it as Roche ellipsoid and the second primary as a triaxial rigid body.
Let the first primary of
mass
be a Roche ellipsoid filled with homogeneous
incompressible fluid of density
and the second primary a triaxial rigid body of mass
outside the ellipsoid. The two infinitesimal bodies
(of mass
and
respectively) are small solid spheres of density
and
respectively inside the ellipsoid. Let
denote the distance between the centres of mass of
and
. Let
describe a circular orbit of radius R around
with constant angular velocity
. The masses
and
mutually attract each other, do not influence the
motions of
and
but are influenced by them.We assume that (i)
and
never reach the surface of the Ellipsoid (ii)their
position vectors at any time
are not the same. Consider a uniformly rotating
coordinate system
with origin of the coordinate system at the centre of
the bigger primary ,
pointing towards
and
being the orbital plane of
around
coinciding with the equatorial plane of
. The coordinate system
is as shown in the Figure 1. Let the synodic system of coordinates initially
coincident with the inertial system rotate with angular velocity
. This is the same as the angular velocity of
which is describing a circle around
. Let initially the principal axes of
be parallel to the synodic axes and their axes of
symmetry be perpendicular to the plane of motion. Since
is revolving without rotation about
with the same angular velocity as that of the synodic
axes, the principal axes of
will remain parallel to them throughout the motion.
The equations of motion of
and
in the Robe’s circular restricted problem of
bodies in the Roche ellipsoid -Triaxial body setup
when perturbations are given to the Coriolis and centrifugal forces are given
by
In this paper, we have
studied the effect of perturbations in the Coriolis and centrifugal forces on
the location and stability of the equilibrium points in Robe’s restricted
problem of 2+2 bodies. Plastino & Plastino (1995) revised the Robe’s
restricted three-body problem under the assumption that the fluid body assumes
the shape of a Roche ellipsoid. They took into consideration all the three
components of the pressure field in deriving the expression for the buoyancy
force viz, due to the own gravitational field of the fluid, that originating in
the attraction of
and that arising from the centrifugal force.They
proved that that the centre of the Roche Ellipsoid viz,
is the only equilibrium solution of the system.The
equilibrium solutions in our case as compared to Plastino & Plastino (1995)
are perturbed along
,
and
axis.We have assumed throughout the paper that the
perturbed coordinates of
and
are such that
and
remain within the Ellipsoid.There exist two
equilibrium solutions of the system lying each on
axis or
axis or
axis. Hence, there exist six equilibrium solutions of
the system, provided they lie within Roche ellipsoid. We observe that there are
no other equilibrium solutions except these six. We observe that the
triaxiality of the second primary and small perturbations in the Coriolis and
centrifugal forces have significant effect on the equations of motion. The
number of equilibrium solutions in this problem are the same as in the problem
with no perturbation (Bhavneet & Rajiv(2013)), but positions of the
equilibrium solutions have changed. The change in the Coriolis force does not
affect the position of the equilibrium solutions. The stability behavior of the
equilibrium solution depends on the sign of the small perturbations in the
Coriolis and centrifugal forces .The equilibrium solutions of
( and similarly of
) lying on
,
,
axis are unstable for
;
and stable for
;
,using the data of submarines in the Earth -Moon
system. Similarly, the equilibrium solutions of
and
respectively when the displacement is given in the
direction of
or
axis are conditionally stable. Earth is the only
celestial body we know of which has fluid and the test particles within the
fluid are considered as the submarines. In the solar or the extra solar system,
we donot know of any other celestial body having liquid inside it. Our entire
work is applicable in solar or extra solar system when and if such a system is discovered.
Table 1ϵ>0 and ϵ'<0
|
|
|
|
|
|
0.02 |
-0.01 |
-4.60675 |
0.000121742 |
|
0.03 |
-0.02 |
-4.68675 |
0.000200461 |
|
0.04 |
-0.03 |
-4.76675 |
0.00027918 |
|
0.05 |
-0.04 |
-4.84675 |
0.000357899 |
|
0.06 |
-0.05 |
-4.92675 |
0.000436617 |
|
0.07 |
-0.06 |
-5.00675 |
0.000515336 |
|
0.08 |
-0.07 |
-5.08675 |
0.000594055 |
|
0.09 |
-0.08 |
-5.16675 |
0.000672774 |
|
0.1 |
-0.09 |
-5.24675 |
0.000751492 |
Table 2ϵ>0 and ϵ'>0
|
|
|
|
|
|
0.02 |
0.01 |
-4.60675 |
-0.0000356952 |
|
0.03 |
0.02 |
-4.68675 |
-0.000114414 |
|
0.04 |
0.03 |
-4.76675 |
-0.000193133 |
|
0.05 |
0.04 |
-4.84675 |
-0.000271851 |
|
0.06 |
0.05 |
-4.92675 |
-0.00035057 |
|
0.07 |
0.06 |
-5.00675 |
-0.000429289 |
|
0.08 |
0.07 |
-5.08675 |
-0.000508008 |
|
0.09 |
0.08 |
-5.16675 |
-0.000586726 |
|
0.1 |
0.09 |
-5.24675 |
-0.000665445 |
Table 3ϵ<0 and ϵ'>0
|
|
|
|
|
|
-0.02 |
0.01 |
-4.28675 |
-0.0000356952 |
|
-0.03 |
0.02 |
-4.20675 |
-0.000114414 |
|
-0.04 |
0.03 |
-4.12675 |
-0.000193133 |
|
-0.05 |
0.04 |
-4.04675 |
-0.000271851 |
|
-0.06 |
0.05 |
-3.96675 |
-0.00035057 |
|
-0.07 |
0.06 |
-3.88675 |
-0.000429289 |
|
-0.08 |
0.07 |
-3.80675 |
-0.000508008 |
|
-0.09 |
0.08 |
-3.72675 |
-0.000586726 |
|
-0.1 |
0.09 |
-3.64675 |
-0.000665445 |
Table 4ϵ<0 and ϵ'<0
|
|
|
|
|
|
-0.02 |
-0.01 |
-4.28675 |
0.000121742 |
|
-0.03 |
-0.02 |
-4.20675 |
0.000200461 |
|
-0.04 |
-0.03 |
-4.12675 |
0.00027918 |
|
-0.05 |
-0.04 |
-4.04675 |
0.000357899 |
|
-0.06 |
-0.05 |
-3.96675 |
0.000436617 |
|
-0.07 |
-0.06 |
-3.88675 |
0.000515336 |
|
-0.08 |
-0.07 |
-3.80675 |
0.000594055 |
|
-0.09 |
-0.08 |
-3.72675 |
0.000672774 |
|
-0.1 |
-0.09 |
-3.64675 |
0.000751492 |
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5. Hallan, P.P. and Rana, N.:2003, ’Effect of Perturbations in the Coriolis and Centrifugal Forces on the Locations and Stability of the Equilibrium Point in the Robe’s Circular Problem with Density Parameter Having Arbitrary Value’, Indian J. pure appl. Math., 34(7), 1045-1059.
6. Hallan, P.P. and Mangang, K.B.:2007, ’Existence and linear stability of equilibrium points in the Robe’s Restricted Three-Body Problem when the first primary is an Oblate Spheroid’, Planetary and Space Science 55, 512-516.
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8. Kaur, Bhavneet and Aggarwal, R.:2013 ’Robe’s restricted problem of 2+2 bodies when the bigger primary is a Roche ellipsoid and the smaller primary is an oblate body’, Astrophysics and Space Science, ISSN 0004-640X, http://dx.doi.org/10.1007/s10509-013-1607-y. Plastino, A.R. & Plastino, A. :1995, ’Robe’s Restricted Three-Body Problem Revisited’, Celestial Mechanics and Dynamical Astronomy 61, 197-206.
9. Robe, H.A.G.:1977, ’A New Kind of Three-Body Problem’, Celestial Mechanics 16, 343-351.
10. Shrivastava, A. K. and Garain, D.: 1991,’Effect of perturbation on the location of libration point in the Robe restricted problem of three bodies’, Celest. Mech. & Dyn. Astr. 51, 67-73.
11. Singh, J. and Mohammed, H.L.:2012, ’Robe’s Circular Restricted Three-Body Problem Under Oblate and Triaxial Primaries’, Earth, Moon, and Planets 109, 1-11.
12. Singh, J. and Sandah, A.U.:2012, ’Existence and Linear Stability of Equilibrium Points in the Robe’s Restricted Three-Body Problem with Oblateness’, Advances in Mathematical Physics, Volume 2012, 18 pages.
13. Singh, J. and Mohammed, H.L.:2013, ’Out-of-plane equilibrium points and their stability in the Robe’s problem with oblateness and triaxiality’, Astrophysics and Space Science 345, 265-271.
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Received on 23.08.2016 Accepted on 08.09.2016 © EnggResearch.net All Right Reserved Int. J. Tech. 2016; 6(2): 150-160. DOI: 10.5958/2231-3915.2016.00024.9 |
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