Journal
CELESTIAL MECHANICS & DYNAMICAL ASTRONOMY
Volume 91, Issue 3-4, Pages 301-322Publisher
SPRINGER
DOI: 10.1007/s10569-004-4622-z
Keywords
symplectic integrators; positive time steps; three-body orbits; long time simulations
Ask authors/readers for more resources
We introduce a class of fourth order symplectic algorithms that are ideal for doing long time integration of gravitational few-body problems. These algorithms have only positive time steps, but require computing the force gradient in addition to the force. We demonstrate the efficiency of these Forward Symplectic Integrators by solving the circular restricted three-body problem in the space-fixed frame where the force on the third body is explicitly time-dependent. These algorithms can achieve accuracy of Runge-Kutta, conventional negative time step symplectic and corrector symplectic algorithms at step sizes five to ten times as large.
Authors
I am an author on this paper
Click your name to claim this paper and add it to your profile.
Reviews
Recommended
No Data Available