Dynamics of tethered satellites in the vicinity of the Lagrangian point L 2 $L_{2}$ of the Earth–Moon system

2017 ◽  
Vol 362 (8) ◽  
Author(s):  
M. F. Baião ◽  
T. J. Stuchi
2013 ◽  
Vol 22 (1) ◽  
pp. 19-22
Author(s):  
MIHAI BARBOSU ◽  
◽  
TIBERIU OPROIU ◽  

This paper presents trajectories of a spacecraft moving in the gravitational field given by Rein’s model for the restricted three-body problem. For various initial conditions, closed orbits are determined using Maple’s numerical capabilities for ODE. Applications to the Earth-Moon system are considered, with trajectories computed around the stable L4 Lagrangian point.


Author(s):  
Yue Wang ◽  
Ruikang Zhang ◽  
Chen Zhang ◽  
Hao Zhang
Keyword(s):  

1998 ◽  
Vol 11 (1) ◽  
pp. 398-398
Author(s):  
Kenji Tanabe

Propagation of the surface waves of the lobe-filing components of close binary systems is investigated theoretically. Such waves are considered to be analogous to the gravity waves of water on the earth. As a result, the equations of the surface wave in the rotating frame of reference are reduced to the so-called Kortewegde Vries (KdV) equation and non-linear Schroedinger (NLS) equation according to its ”depth”. Each of these equations is known to have the solution of soliton. When this soliton is sent to the other component of the binary system through the Lagrangian point, it can give rise to the flare activity observed in some kinds of close binary systems.


2001 ◽  
Vol 45 (11) ◽  
pp. 922-928 ◽  
Author(s):  
G. S. Kurbasova ◽  
L. V. Rykhlova

1967 ◽  
Vol 13 (5) ◽  
pp. 545-546 ◽  
Author(s):  
T. F. Gaskell
Keyword(s):  

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