Pages that link to "Item:Q2229675"
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The following pages link to Explicit symplectic integrator for highly eccentric orbits (Q2229675):
Displaying 7 items.
- Symplectic integrators and their application to dynamical astronomy (Q758245) (← links)
- Numerical integration of relativistic equations of motion for Earth satellites (Q1011852) (← links)
- A note on the use of generalized Sundman anomalies in the numerical integration of the elliptical orbital motion (Q1724754) (← links)
- Methods for the Study of the Dynamics of the Oort Cloud Comets II: Modelling the Galactic Tide (Q3613188) (← links)
- On the symmetric difference quotient and its application to the correction of orbits (II). A numerical analysis (Q3817692) (← links)
- (Q3842146) (← links)
- Improved leap-frog symplectic integrators for orbits of small eccentricity in the perturbed Kepler problem (Q5955278) (← links)