MOTION NEAR THE TRIANGULAR POINTS IN THE ELLIPTIC RESTRICTED PROBLEM OF 3 BODIES

被引:1
作者
CHENG, BK
机构
[1] Departmento de Física, Setor de Ciências Exatas, Universidade Federal do Paraná, Curitiba
来源
CELESTIAL MECHANICS | 1979年 / 19卷 / 01期
关键词
D O I
10.1007/BF01230172
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
In this paper the first variational equations of motion about the triangular points in the elliptic restricted problem are investigated by the perturbation theories of Hori and Deprit, which are based on Lie transforms, and by taking the mean equations used by Grebenikov as our upperturbed Hamiltonian system instead of the first variational equations in the circular restricted problem. We are able to remove the explicit dependence of transformed Hamiltonian on the true anomaly by a canonical transformation. The general solution of the equations of motion which are derived from the transformed Hamiltonian including all the constant terms of any order in eccentricity and up to the periodic terms of second order in eccentricity of the primaries is given. © 1979 D. Reidel Publishing Co.
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页码:31 / 41
页数:11
相关论文
共 11 条
[1]  
ALFRIEND KT, 1968, J ASTRONAUT SCI, V15, P105
[2]  
AOKI S, 1955, PUBL ASTRON SOC JAPA, V7, P105
[3]   CHARACTERISTIC EXPONENTS OF 5 EQUILIBRIUM SOLUTIONS IN ELLIPTICALLY RESTRICTED PROBLEM [J].
BENNETT, A .
ICARUS, 1965, 4 (02) :177-&
[4]   STABILITY OF TRIANGULAR POINTS IN ELLIPTIC RESTRICTED PROBLEM OF 3 BODIES [J].
DANBY, JMA .
ASTRONOMICAL JOURNAL, 1964, 69 (02) :165-&
[5]  
DEPRIT A, 1970, J ASTRON ASTROPHYS, V5, P416
[6]  
Grebenikov E. A., 1964, SOV ASTRON, V8, P451
[7]  
HORI G., 1966, PUBL ASTRON SOC JAPA, V18, P287
[8]   STABILITY OF TRIANGULAR POINTS IN ELLIPTIC RESTRICTED PROBLEM OF 3 BODIES [J].
NAYFEH, AH ;
KAMEL, AA .
AIAA JOURNAL, 1970, 8 (02) :221-&
[9]  
Szebehely V., 1967, THEORY ORBITS
[10]  
Tschauner J., 1974, Celestial Mechanics, V9, P419, DOI 10.1007/BF01329324