Restricted Three Body Problem with Stokes Drag Effect
نویسندگان
چکیده
منابع مشابه
The Restricted Three Body Problem with Quadratic Drag
When an asteroid, space-craft or another small object in the solar system is in the vicinity of a planet it is subjected to the gravitational forces of the Sun, the planet, the drag forces due to the solar wind and (possibly) the planet upper atmosphere. To determine the object trajectory we consider this problem within the context of the restricted three body problem in three dimensions with q...
متن کاملCaustics of the restricted three-body problem
Trajectories of the planar, circular, restricted threebody problem are given in the configuration space through the caustics associated to the invariant tori of quasi-periodic orbits. It is shown that the caustics of trajectories librating in any particular resonance display some features associated to that resonance. This method can be considered complementary to the Poincaré surface of sectio...
متن کاملPeriodic Orbits of a Collinear Restricted Three Body Problem
In this paper we study symmetric periodic orbits of a collinear restricted three body problem, when the middle mass is the largest one. These symmetric periodic orbits are obtained from analytic continuation of symmetric periodic orbits of two collinear two body problems.
متن کاملAn Analysis of Stability in the Restricted Three-body Problem
The three body problem studies the motion of three masses whose gravitational attraction have an effect on each other. The dynamics of the three body problem are essentially different from those of two bodies, because in the latter case, an analytical solution may be found that admits orbits in the form of conic sections. This problem has been studied at great length and is the basis of most of...
متن کاملGlobal instability in the elliptic restricted three body problem∗
The (planar) ERTBP describes the motion of a massless particle (a comet) under the gravitational field of two massive bodies (the primaries, say the Sun and Jupiter) revolving around their center of mass on elliptic orbits with some positive eccentricity. The aim of this paper is to show that there exist trajectories of motion such that their angular momentum performs arbitrary excursions in a ...
متن کاملذخیره در منابع من
با ذخیره ی این منبع در منابع من، دسترسی به آن را برای استفاده های بعدی آسان تر کنید
ژورنال
عنوان ژورنال: International Journal of Astronomy and Astrophysics
سال: 2015
ISSN: 2161-4717,2161-4725
DOI: 10.4236/ijaa.2015.52013