Invariantmanifolds near L1 and L2 in the Sun-Jupiter elliptic restricted three-body problem II: the dynamics of comet Oterma

被引：0

作者：

Duarte, Gladston ^{[1
,2
]}

Jorba, Angel ^{[2
,3
]}

机构：

[1] Univ Torino, Dipartimento Matemat, Via Carlo Alberto 10, I-10123 Turin, Italy

[2] Univ Barcelona, Dept Matemat & Informat, Gran Via Corts Catalanes 585, Barcelona 08007, Spain

[3] Ctr Recerca Matemat, Edif C,Campus Bellaterra, Bellaterra 08193, Spain

来源：

CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY | 2024年 / 136卷 / 06期

关键词：

Planar elliptic restricted three-body problem; Lagrangian points; Rapid transition mechanism; Comet; 39P/Oterma; NORMAL BEHAVIOR; CAPTURE; TORI;

D O I：

10.1007/s10569-024-10218-y

中图分类号：

P1 [天文学];

学科分类号：

0704 ;

摘要：

Comet 39P/Oterma is known to make fast transitions between heliocentric orbits outside the orbit of Jupiter and heliocentric orbits inside that of Jupiter. In this paper, the dynamics of comet Oterma is modelled and fitted in the Planar Elliptic RTBP. Using the computations presented in Duarte(Celest. Mech. Dyn. Astron 136:26, 2024), we look for the invariant objects around L-1 and L-2, which in the case of the Planar Elliptic RTBP is invariant tori and their stable and unstable manifolds that are the skeleton that guides Oterma in its rapid transition.

引用

页数：20

共 41 条

[1] Invariant manifolds near L1 and L2 in the Sun-Jupiter elliptic restricted three-body problem I
Duarte, Gladston
Jorba, Angel
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2024, 136 (04):
[2] Halo orbits around L1, L2, and L3 in the photogravitational Sun-Mars elliptical restricted three-body problem
Sheth, Dhwani
Thomas, V. O.
ASTROPHYSICS AND SPACE SCIENCE, 2022, 367 (10)
[3] Structure of the centre manifold of the L1, L2 collinear libration points in the restricted three-body problem
Pucacco, Giuseppe
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 2019, 131 (10):
[4] Interplanetary transfers using stable and unstable manifold tubes originating at L1 and L2 in the elliptic restricted three-body problems
Scantamburlo, Erica
Guzzo, Massimiliano
Paez, Rocio Isabel
ACTA ASTRONAUTICA, 2022, 200 : 97 - 110
[5] Interplanetary transfers using stable and unstable manifold tubes originating at L1 and L2 in the elliptic restricted three-body problems
Scantamburlo, Erica
Guzzo, Massimiliano
Paez, Rocio Isabel
Acta Astronautica, 2022, 200 : 97 - 110
[6] Transits close to the Lagrangian solutions L 1, L 2 in the elliptic restricted three-body problem
Paez, Rocio, I
Guzzo, Massimiliano
NONLINEARITY, 2021, 34 (09) : 6417 - 6449
[7] PERIODIC SOLUTIONS AROUND THE COLLINEAR LANGRANGIAN POINTS IN THE PHOTOGRAVITATIONAL RESTRICTED THREE-BODY PROBLEM: SUN-JUPITER CASE
Ragos, O.
Zagouras, C.
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1990, 50 (04): : 325 - 347
[8] A study of halo orbits at the Sun–Mars L1 Lagrangian point in the photogravitational restricted three-body problem
Roshan Thomas Eapen
Ram Krishan Sharma
Astrophysics and Space Science, 2014, 352 : 437 - 441
[9] Regularization of the restricted elliptic three-body problem in the sun-earth L1-centered rotating system
Kechichian, JA
ASTRODYNAMICS 2001, PTS I-III, 2001, 109 : 367 - 387
[10] A study of halo orbits at the Sun-Mars L1 Lagrangian point in the photogravitational restricted three-body problem
Eapen, Roshan Thomas
Sharma, Ram Krishan
ASTROPHYSICS AND SPACE SCIENCE, 2014, 352 (02) : 437 - 441

← 1 2 3 4 5 →