Discussion on Geodynamics of Three-body Motion

2015 ◽  
Vol 89 (6) ◽  
pp. 1858-1864
Author(s):  
LIU Quanwen ◽  
YAN Lingling ◽  
CHEN Guomin
Keyword(s):  
Author(s):  
Jeremy Gray

Leonhard Euler’s importance for the history of mathematics is undoubted. Not only was he the most prolific mathematician ever – his collected works so far run to 76 volumes and further editions of his correspondence are planned – he dominated the eighteenth century. He combined an extraordinary memory, a capacity for a huge range of interests, an exceptional technical facility, and an ability to work to a high level of abstraction with a natural clarity of expression. His importance extends beyond his many profound innovations in many fields, of which three can be mentioned here: - mechanics, which he built up from the motion of point masses through the theory of rigid body motion to aero- and hydrodynamics, with applications to ship design, gunnery, optics, and celestial mechanics, where he did important work on the motion of the Moon and the three body problem; - the calculus, where he successfully introduced the concept of a function as fundamental; and - number theory, including the theory of quadratic forms and the zeta function. It was also the force of his example that established the culture of publishing in mathematics, and replaced the markedly more secretive habits of Newton and Leibniz. His widespread correspondence stimulated others, his work at the head of the Academy of St Petersburg helped develop mathematics in Russia, and his textbooks on the differential and integral calculus and on algebra made the subject accessible to generations of students.


2014 ◽  
Vol 926-930 ◽  
pp. 3084-3087
Author(s):  
Hao Yang Li ◽  
Zhi Kun She ◽  
Bai Xue ◽  
Wang Jie Qiu ◽  
Zhi Ming Zheng

This paper analyzes the restricted three-body problems in the ground test systems. First, under the ideal condition, after analyzing the forces on the spacecraft in the rotating coordinates, a mathematical model of elliptic restricted three-body motion is founded. Second, for the restricted three-body problem in the ground test system, the forces on the test ball are analyzed and the corresponding elliptic mathematical model apart from the perturbation is founded. Then, based on the two models founded above, the similarity between the ideal spatial model and the ground simulation model is analyzed.


2018 ◽  
Vol 168 ◽  
pp. 04001
Author(s):  
Medeu Abishev ◽  
Saken Toktarbay ◽  
Aigerim Abylayeva ◽  
Amanhan Talkhat

We investigate the orbital stability of a test particle motion in the restricted three-body problem where all bodies have their own rotation. We have shown that it is possible to get some insight into the stability properties of the motion of test particles in restricted three-body problem, without knowing the exact solutions of the relativistic motion equations.


Aerospace ◽  
2021 ◽  
Vol 8 (3) ◽  
pp. 68
Author(s):  
Giordana Bucchioni ◽  
Mario Innocenti

The paper presents the development of a fully-safe, automatic rendezvous strategy between a passive vehicle and an active one orbiting around the Earth–Moon L2 Lagrangian point. This is one of the critical phases of future missions to permanently return to the Moon, which are of interest to the majority of space organizations. The first step in the study is the derivation of a suitable full 6-DOF relative motion model in the Local Vertical Local Horizontal reference frame, most suitable for the design of the guidance. The main dynamic model is approximated using both the elliptic and circular three-body motion, due to the contribution of Earth and Moon gravity. A rather detailed set of sensors and actuator dynamics was also implemented in order to ensure the reliability of the guidance algorithms. The selection of guidance and control is presented, and evaluated using a sample scenario as described by ESA’s HERACLES program. The safety, in particular the passive safety, concept is introduced and different techniques to guarantee it are discussed that exploit the ideas of stable and unstable manifolds to intrinsically guarantee some properties at each hold-point, in which the rendezvous trajectory is divided. Finally, the rendezvous dynamics are validated using available Ephemeris models in order to verify the validity of the results and their limitations for future more detailed design.


1978 ◽  
Vol 41 ◽  
pp. 356-356
Author(s):  
Jörg Waldvogel

AbstractThe family of trajectories near a triple collision solution in the planar problem of three bodies is investigated by means of linearization in the neighborhood of the parabolic free fall. The local topological structure of this family is found to be that of a saddle point in the R8. The corresponding stable manifold is the set of all triple collision solutions, whereas the instable manifold is formed by the parabolic solutions.In important cases of nonzero total energy the family of close encounters is quantitatively described in terms of hypergeometric functions. By means of homothetic transformations the close triple encounters are then related to three-body motion with zero energy and zero angular momentum. In this way almost all close encounters near a homothetic solution can be treated by using a small number of particular solutions of the three-body problem that may be calculated once for all.In practical examples the first order theory presented here predicts the escape velocity after a close triple encounter with a relative accuracy comparable to the closeness of the encounter.


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