Evolution of periodic orbits near the Lagrangian point L2

被引:11
作者
Dutt, Pooja [1 ]
Sharma, R. K. [1 ]
机构
[1] ISRO, Vikram Sarabhai Space Ctr, Div Appl Math, Thiruvananthapuram 695022, Kerala, India
关键词
Astrodynamics; Planar circular restricted three-body problem; Poincare surface of section; Periodic and quasi-periodic orbits; Third- and fourth-order resonances; Separatrix; Lagrangian point L-2; RESTRICTED PROBLEM; STABILITY; MOON;
D O I
10.1016/j.asr.2011.01.024
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A study of the evolution of the periodic and the quasi-periodic orbits near the Lagrangian point L-2, which is located to the right of the smaller primary on the line joining the primaries and whose distance from the more massive primary is greater than the distance between the primaries, in the framework of restricted three-body problem for the Sun-Jupiter, Earth-Moon (relatively large mass ratio) and Saturn-Titan (relatively small mass ratio) systems is made. Two families of periodic orbits around the smaller primary are identified using the Poincare surface of section method - family I (initially elliptical, gradually becomes egg-shaped with the increase in the Jacobi constant C and elongated towards the more massive primary) and family II (initially egg-shaped orbits elongated towards L-2 and gradually becomes elliptical with the increase in C). The family I in the Sun-Jupiter and Saturn-Titan systems contains two separatrix caused by third-order and fourth-order resonances, while the Earth-Moon system has only one separatrix which is caused by third-order resonances. Also in the Sun-Jupiter and the Saturn-Titan systems, family I merge with family II, around Jacobian constant 3.0393 and 3.0163, respectively, while in the Earth-Moon system, family II evolves separately from two different branches. The two branches merge at C = 3.184515. In the Earth-Moon system, the family II contains a separatrix due to third-order resonances which is absent in the other two systems. (C) 2011 COSPAR. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:1894 / 1904
页数:11
相关论文
共 12 条
[1]  
Arnold V. I., 1980, MATH METHODS CLASSIC
[2]   Effect of radiation on the stability of a retrograde particle orbit in different stellar systems [J].
Das, M. K. ;
Narang, Pankaj ;
Mahajan, S. ;
Yuasa, M. .
PLANETARY AND SPACE SCIENCE, 2009, 57 (07) :836-845
[3]   Effects of resonances on the stability of retrograde satellites [J].
Douskos, C. ;
Kalantonis, V. ;
Markellos, P. .
ASTROPHYSICS AND SPACE SCIENCE, 2007, 310 (3-4) :245-249
[4]  
DUTT P, 2011, J GUIDANCE CONTROL D, V34
[5]   Analysis of Periodic and Quasi-Periodic Orbits in the Earth-Moon System [J].
Dutt, Pooja ;
Sharma, R. K. .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2010, 33 (03) :1010-1017
[6]  
HENON M, 1970, ASTRON ASTROPHYS, V9, P24
[7]  
JEFFERYS WH, 1971, ATLAS SURFACES SECTI, V3, P6
[8]   STATIONARY SOLUTIONS AND THEIR CHARACTERISTIC EXPONENTS IN RESTRICTED 3-BODY PROBLEM WHEN MORE MASSIVE PRIMARY IS AN OBLATE SPHEROID [J].
SHARMA, RK ;
RAO, PVS .
CELESTIAL MECHANICS, 1976, 13 (02) :137-149
[9]   THE ONSET OF CHAOTIC MOTION IN THE RESTRICTED PROBLEM OF THREE BODIES [J].
Smith, R. H. ;
Szebehely, V. .
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY, 1993, 56 (03) :409-425
[10]  
Szebehely V., 1967, RESTRICTED PROBLEM 3