The total angular-momentum plane in the nonrelativistic three-body problem

1963 ◽  
Vol 29 (2) ◽  
pp. 400-419 ◽  
Author(s):  
R. G. Newton
1989 ◽  
Vol 6 (2) ◽  
pp. 97-113 ◽  
Author(s):  
V. V. Kostrykin ◽  
A. A. Kvitsinsky ◽  
S. P. Merkuriev

2001 ◽  
Vol 10 (01) ◽  
pp. 69-82 ◽  
Author(s):  
XIAO-YAN GU ◽  
BIN DUAN ◽  
ZHONG-QI MA

We demonstrate explicitly how the rotational degrees of freedom in a quantum three-body problem is separated completely from the internal ones. It is shown that only finite partial angular momentum states are involved in constructing the base-functions with the given angular momentum and parity, and the contributions by the remaining partial angular momentum states are incorporated into the contributions by the generalized radial functions.


1989 ◽  
Vol 17 (4) ◽  
pp. 307-313 ◽  
Author(s):  
S. P. Merkuriev ◽  
A. A. Kvitsinsky

1973 ◽  
Vol 33 (2) ◽  
pp. 243-266 ◽  
Author(s):  
E. El Baz ◽  
C. Fayard ◽  
G -H. Lamot ◽  
J. Pigeon

2007 ◽  
Vol 27 (6) ◽  
pp. 1933-1946 ◽  
Author(s):  
RICHARD MONTGOMERY

AbstractA syzygy in the three-body problem is a collinear instant. We prove that, with the exception of Lagrange’s solution, every solution to the zero angular momentum, Newtonian three-body problem suffers syzygies. The proof works for all mass ratios.


2021 ◽  
Vol 57 (2) ◽  
pp. 445-457
Author(s):  
A. F. S. Ferreira ◽  
R. V. de Moraes ◽  
A. F. B. A. Prado ◽  
O. C. Winter ◽  
V. M. Gomes

The present paper surveys the more recent techniques related to the swingby maneuver, where a spacecraft changes its energy and angular momentum by passing close to celestial bodies. It is focused on the literature related to extensions of this maneuver, with emphasis in the powered version, where an impulse is applied to the spacecraft near the closest approach. Several mathematical models are considered, including the patched-conics approximation for analytical studies, and the restricted three-body problem for the numerical simulations. The main goal is to show the models and the main conclusions available in the literature for those maneuvers. Some key results are shown to discuss important aspects of this maneuver, including the analysis of the energy variation of the spacecraft, the behavior of the trajectories and other applications.


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