R C
O S T N
Publisher: Research Council of Science and Technology, Biratnagar, Nepal p. 53
BIBECHANA
A Multidisciplinary Journal of Science, Technology and Mathematics
ISSN 2091-0762 (print), 2382-5340 (online)
Journal homepage: http://nepjol.info/index.php/BIBECHANA
Energy of Sitnikov's restricted three body problem if the
primaries are source of radiation and triaxial rigid bodies
R.R.Thapa1,2*
1
University Department of Mathematics., T.M. Bhagalpur University, Bhagalpur, India
2
P.G. Department of Mathematics., P.G. Campus, Biratnagar, T.U., Nepal. *E-mail: thaparajuram@yahoo.com
Accepted for publication: December 13, 2014
Abstract
In this paper the joint effect of source of radiation and triaxial rigid body has been studied. The energy of Sitnikov's restricted three body problem when primaries are sources of radiation and energy of Sitnikov's restricted problem of three bodies when primaries are triaxial rigid bodies have been studied to calculate the joint effect. Equation of motion of the third body of infitesimal mass, if primaries are sources of radiation and triaxial rigid bodies, are calculated.
DOI: http://dx.doi.org/10.3126/bibechana.v12i0.11707 © 2014 RCOST: All rights reserved.
Keywords: Dimensional distance; oscillatory motion; periodicity; radiation parameter.
1. Introduction
Sitnikov [1] problem can be integrated in case of restricted problem if primaries are taken to be equal masses. If primaries are triaxial rigid bodies then distance between them will be changed. Then third body can move along z axis. But if primaries are sources of radiation then the third body moves along the line perpendicular through the centre of mass of the primaries and is perpendicular to the plane of motion.
Thapa et al. [2] obtained the periodicity of Sitnikov's restricted three body problem when the
primaries are sources of radiation. They found the equations of motion of the third body and total energy of the system. R.R. Thapa et al. [3] also obtained the equations of motion of the Sitnikov's restricted problem of three bodies when Primaries are triaxial rigid bodies. They got the equations of motion in dimensionless variables and Cartesian form as
2
2
x
y
x
ny
y
nx
z
−
= Ω
+
= Ω
= Ω
ɺɺ
ɺ
ɺɺ
ɺ
Thapa/ BIBECHANA 12 (2015) 53-58: p. 54
2
2 2 1 2
3
1 2 1
2
1 2 1 2
3 5
2 1
2 2 2
1 2 1 1
5 5 5
2 1 2
(1 )(2 ) 1
where ( )
2 2
(2 ) 3(1 )( )
2 2
3 ( ) 3(1 ) 3
2 2 2
− −
−
Ω = + + + +
′− ′ − −
+ −
′− ′ − ′
− − −
n x y
r r r
y
r r
y z z
r r r
µ σ σ
µ µ
µ σ σ µ σ σ
µ σ σ µ σ µσ
In present work we have proposed to get the energy of restricted three body problem if the primaries are source of radiation and triaxial rigid bodies.
2. Equation of motion
We will adopt the notation and terminology of szehebely [4].
We have the equation of motion of the third body of infinitesimal mass is
3
1 2 1 2 1 1
3 5 7
2 2 2 2 2 2
2 2 2
3(2 2 ) 15( )
(1 )
4 4
4 4 4
σ σ
− +σ
′−σ
′σ
+σ
′∂Ω − −
= = − +
∂
+ + +
ɺɺz p z z z
z
a a a
z z z
3 2
1 1
3 5 7
2
2 2 2 2 2 2
2 2 2
( )
(1 ) 3 15
4 4
4 4 4
σ
σ
α
+ ′− −
= − +
+ + +
z
d z p z z
dt
a a a
z z z
(1)
where
α
=2σ
1−σ
2+2σ
1′−σ
2′Equation (1) is non-linear equation. It can be integrated by linearizing it.
3. Energy of the third body
If we multiply (1) by2dz
dt we get,
3 2
1 1
3 5 7
2
2 2 2 2 2 2
2 2 2
15( )
2(1 ) 3 2
2 2
4 4
4 4 4
′ + −
= − − × +
+ + +
z
dz d z p z dz dz dz
z
dt dt dt dt dt
a a a
z z z
σ σ
α
Or,
2 2
2 2
1 1
3 5 7
2 2 2 2 2 2
2 2 2
4 4
15( )
1 (1 ) 3
2 4
4
4 4 4
+ −
′ + −
= − − × +
+ + +
a a
z z
d dz p z dz z dz dz
dt dt dt dt dt
a a a
z z z
σ σ
α
Thapa/ BIBECHANA 12 (2015) 53-58: p. 55
2
1 1
3 5 5 7
2 2 2 2 2 2 2 2
2 2 2 2
15( )
(1 ) 3
4 4
4
4 4 4 4
′ + − − − + − + + + +
p z dz z dz z dz a z dz
dt dt dt dt
a a a a
z z z z
σ σ
α (2)
If we substitute udu zdz dt = dt and
2
2 2
4
a
u = z + we get,
( )
( )
( )
( )
2 2
1 1
3 5 5 7
2 2 2 2 2 2 2 2
2
1 1
2 4 4 6
1 1 1 1
2 4 4
15( )
1 (1 ) 3 1 1
2 4 4
4
15( )
(1 ) 3 1 1 1
4 4 4
1 3 15 1 15
( ) (
4 4 4
′ + − = − − + − ′ + − = − − + − ′ ′ = − − + + − +
d dz p du du du a du
u u u u
dt dt dt dt dt dt
u u u u
p du du du du
a
u dt u dt u dt u dt
du du du
u dt u dt u dt
σ σ α σ σ α α σ σ σ σ
( )
2 6 21 3 3
5
1 1 1 1
1 )
4
5( ) 3( )
(1 )
4 4 16
− − − − ⋅ ′ ′ + + − = + − + a du u dt a
p du du du d
u
dt dt dt dt
σ σ σ σ
α
2 1 3 3 2 5
1 1 1 1
2 2
1 3 3 1 1 5
1 1
2
1 1 1 1
3 3
5( ) 3( )
1
(1 )
2 4 4 16
3( )
1 5
(1 ) ( )
2 4 4 16
5( ) 3( )
1 (1 )
2 4 4
− − − − − − − − ′ ′ + + = − + − ′ + ′ ⇒ = − + − + + + ′ ′ + + − ⇒ = + − +
∫
d dz dt p∫
du dt∫
du dt∫
du dt a∫
du dtdt dt dt dt dt dt
a dz
p u u u u c
dt
a
dz p
dt u u u
σ
σ
σ
σ
α
σ
σ
α
σ
σ
σ
σ
σ
σ
α
2 5 2 21 1 1 1
3 3 5
2
2 2 2 2 2 2
2
2 2 2
2 2
1 1 1 1
3 3
2
2 2 2 2 2
2
2 2 2
1 16
5( ) 3( )
1 (1 )
2
4 4 16
4 4 4 4
5( ) 3( )
1 (1 )
2
4 4 16
4 4 4 4
+ ′ ′ + + − ⇒ = + − + + + + + + ′ ′ + + − ⇒ − − + − + + + + c u a dz p c dt a
a a a
z z z z
a
dz p
dt a
a a a
z z z z
σ
σ
σ
σ
α
σ
σ
σ
σ
α
5 2 =c(
)
2 21 1 1 2 1 2 1 1
3 5
2
2 2 2 2
2
2 2
5 5 2 2 3( )
1 (1 )
2
4 16
4 4 4
′ ′ ′ + − + − + + ′ − ⇒ − + − = + + + a dz p c dt a a a
z z z
Thapa/ BIBECHANA 12 (2015) 53-58: p. 56
(
)
2 2
1 2 1 2 1 1
3 5
2
2 2 2 2
2
2 2
3 3 3( )
1 (1 )
2
4 16
4 4 4
′ ′ + + + + ′ − ⇒ − + − = + + + a dz p c dt a a a
z z z
σ σ
σ σ
σ σ
2 2
1 1
1 3 5
2 2 2 2 2 2
2 2 2
3( )
1 (1 )
constant 2
4 16
4 4 4
σ
+σ
′ − ⇒ − + − = + + + adz p p
dt
a a a
z z z
2 2
1 1
1 3 5
2 2 2 2 2 2
2 2 2
2
1 1
3 5
2
2 2 2 2
2
2 2
3( )
1 (1 )
constant. 2
4 16
4 4 4
3( )
1 (1 )
constant. 2
4 16
4 4 4
σ
σ
σ
σ
′ + − = − + − = + + + ′ + − = − + − = + + + adz p p
E
dt
a a a
z z z
dz p p
E
dt a
a a
z z z
Now from equation (1)
2
3
1 1
3 5 7
2
2 2 2 2 2 2
2 2 2
2
3
1 1
3 5 7
2
3 2 5 2 7 2
2 2 2
2 2 2
2
2 3
15( )
(1 ) 3
0
4 4
4 4 4
15( )
(1 ) 3
0
4 4 4
1 4 1 4 1
2 2 2
(1 )8
σ
σ
α
σ
σ
α
′ + − + + − = + + + ′ + − ⇒ + + − = + + + − ⇒ +d z p z z
z dt
a a a
z z z
d z p z z
z dt
a z a z a z
a a a
d z p z
dt a
3 5
2 2 2 2
2 5 2
7
3 2 2
1 1
7 2
4 24 4
1 1
15( ) 32 4
1 0
(as so 1)
α
σ
σ
− − − + + + ′ + × − + = << <<<
z z z
a a a
z z
a a
z
z a
a
2 2 2
2
3
1 1
2 3 5 7
(1 )8 3 2 24 5 2 15 32 7 2
1 ... 1 ... ( ) 1 ... 0
2 2 2
− × ′
⇒ + − + + − + − + − + =
d z p z z z z z
z
dt a a a a a a
α
σ σ
Thapa/ BIBECHANA 12 (2015) 53-58: p. 57
(
)
2
2 2
3
1 1
2 3 3 5 5 2 7
2 3
1 1
7 2
2
3
1 1
2 3 5 5 7 7
2
2 2
2 5 7
480( )
(1 )8 8 12 24 24 5 4
2 2
480( ) 7 4
0 2
480( )
(1 )8 24 48 240
... 0
8(1 ) 48
3 5 1
d z p z z z z z z
z
dt a a a a a a a
z z
a a
d z p
z z
dt a a a a a
d z p
a z a
dt a a
σ
σ
α
α
σ
σ
σ
σ
α
α
α
α
′ +
− ×
+ − ⋅ + − × −
′
+
+ × =
′ +
−
+ + − + + + =
−
+ + −
(
+ +)
31 1
0(
σ
+σ
′) z =0
2
2 3
0 0
d z
z z
dt +
η
−ε
= (4)(
)
22 2
0 5 5
2
1 1
7
8(1 ) 8 ( 3 )
where 3
48
and 5 10( )
p q a
a
a a
a a
α
η
α
ε
α
σ
σ
− +
= + =
′
= + + +
The equations (3), (4) represent energy of Sitnikov's restricted three body problem if the primaries are source of radiation and triaxial rigid bodies.
4. Result and Discussion
The energy of third body depends on variable z, radiation parameter p, (parameter) α
=2σ1−σ2+2σ11−σ21, distance between the primaries a; where
2 2
1 3
1 2
a a
, 5R
− σ =
2 2 2 2 2 2
2 1
2 3 1 3 2 3
2 2 1 2 2 2
a a b b b b
, ,
5R 5R 5R
− − −
σ = σ = σ = ; R is dimensional distance between the
primaries and a1,a2,a3; b1,b2,b3are lengths of semi-axes of two primaries parallel to axes
respectively. The kinetic energy of the third body depends on variable z but potential energy depends
on η0 and ε.
where 5
2 2 0
a ) 3 a ( q
8 + α
=
η and [(a 5 10( )]
a
48 2 1
7 + α+ σ+σ
=
ε .
Hence the third body will perform oscillatory motion.
Acknowledgement
I want to acknowledge with thanks my supervisor Dr. M.R. Hassan, Department of Mathematics, S.M. College, Bhagalpur, T.M.B.U. Bghagalpur, 812007, India for his meticulous guidance during the work.
Thapa/ BIBECHANA 12 (2015) 53-58: p. 58
References
[1] K.A. Sitnikov, Dokl. Akad, Nauk, USSR 132(2) (1960) 303.
[2] R.R. Thapa, and M.R. Hassan, Journal of the Bihar Mathematical society 27(2013) 99-105.