CHARACTERISTIC EXPONENTS OF 5 EQUILIBRIUM SOLUTIONS IN ELLIPTICALLY RESTRICTED PROBLEM

被引:62
作者
BENNETT, A
机构
关键词
D O I
10.1016/0019-1035(65)90060-6
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
引用
收藏
页码:177 / &
相关论文
共 6 条
[1]   STABILITY OF TRIANGULAR POINTS IN ELLIPTIC RESTRICTED PROBLEM OF 3 BODIES [J].
DANBY, JMA .
ASTRONOMICAL JOURNAL, 1964, 69 (02) :165-&
[2]  
FADDEEVA VN, 1959, COMPUTATIONAL METHOD, P177
[3]   ON THE ELLIPTIC CASE OF THE RESTRICTED PROBLEM OF 3 BODIES AND THE REMOTE HISTORY OF THE EARTH-MOON SYSTEM [J].
KOPAL, Z ;
LYTTLETON, RA .
ICARUS, 1963, 1 (5-6) :455-458
[4]   On the stability of direct and retrograde satellite orbits. [J].
Moulton, FR .
MONTHLY NOTICES OF THE ROYAL ASTRONOMICAL SOCIETY, 1914, 75 (01) :0040-0057
[5]   ON ELLIPTIC RESTRICTED PROBLEM OF 3 BODIES [J].
SZEBEHELY, VG ;
GIACAGLIA, GE .
ASTRONOMICAL JOURNAL, 1964, 69 (03) :230-+
[6]  
WINTNER A, 1947, ANALYTICAL FOUNDATIO