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Volumn 10, Issue 4, 2005, Pages 261-269
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A symplectic exponentially fitted modified Runge-Kutta-Nyström method for the numerical integration of orbital problems
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Author keywords
Exponential fitting; Long term prediction of earth satellite orbits; Modified Runge Kutta Nystr m methods; Orbit problems; Symplectic integration
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Indexed keywords
ASTRONOMY;
FUNCTIONS;
HAMILTONIANS;
INITIAL VALUE PROBLEMS;
MATRIX ALGEBRA;
ORDINARY DIFFERENTIAL EQUATIONS;
PROBLEM SOLVING;
RUNGE KUTTA METHODS;
THEOREM PROVING;
EXPONENTIAL FITTING;
LONG-TERM PREDICTION OF EARTH SATELLITE ORBITS;
MODIFIED RUNGE-KUTTA NYSTRÖM METHODS;
ORBIT PROBLEMS;
SYMPLETIC INTEGRATION;
ORBITS;
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EID: 14044267389
PISSN: 13841076
EISSN: None
Source Type: Journal
DOI: 10.1016/j.newast.2004.12.004 Document Type: Article |
Times cited : (114)
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References (22)
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