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The co-orbital restricted three-body problem and its application.
- Source :
- SCIENCE CHINA Physics, Mechanics & Astronomy; Jan2010, Vol. 53 Issue 1, p171-178, 8p
- Publication Year :
- 2010
-
Abstract
- Based on large quantities of co-orbital phenomena in the motion of natural bodies and spacecraft, a model of the co-orbital restricted three-body problem is put forward. The fundamental results for the planar co-orbital circular restricted three-body problem are given, which include the selection of variables and equations of motion, a set of approximation formulas, and an approximate semi-analytical solution. They are applied to the motion of the barycenter of the planned gravitational observatory LISA constellation, which agrees very well with the solution of precise numerical integration. [ABSTRACT FROM AUTHOR]
Details
- Language :
- English
- ISSN :
- 16747348
- Volume :
- 53
- Issue :
- 1
- Database :
- Complementary Index
- Journal :
- SCIENCE CHINA Physics, Mechanics & Astronomy
- Publication Type :
- Academic Journal
- Accession number :
- 49697672
- Full Text :
- https://doi.org/10.1007/s11433-010-0110-5