메뉴 건너뛰기




Volumn 10, Issue 4, 2005, Pages 261-269

A symplectic exponentially fitted modified Runge-Kutta-Nyström method for the numerical integration of orbital problems

Author keywords

Exponential fitting; Long term prediction of earth satellite orbits; Modified Runge Kutta Nystr m methods; Orbit problems; Symplectic integration

Indexed keywords

ASTRONOMY; FUNCTIONS; HAMILTONIANS; INITIAL VALUE PROBLEMS; MATRIX ALGEBRA; ORDINARY DIFFERENTIAL EQUATIONS; PROBLEM SOLVING; RUNGE KUTTA METHODS; THEOREM PROVING;

EID: 14044267389     PISSN: 13841076     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.newast.2004.12.004     Document Type: Article
Times cited : (114)

References (22)


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.