CHINESE JOURNAL OF COMPUTATIONAL PHYSICS ›› 1992, Vol. 9 ›› Issue (S2): 810-811.
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Liu Lin, Liao Xinhao
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Abstract: The accuracy of orbital seminajor axis is improved by the energy relation so that the growth of the along-track error in traditional integrators can be controlled. This is called numerical stabilization. The change of step-size can be solved by the transformation of time variable: df=r3/2ds.
Liu Lin, Liao Xinhao. THE PROBLEM OF NUMERICAL STABILIZATION AND STEP-SIZE UNIFORMIZATION IN THE NUMERICAL SOLUTION OF CELESTIAL MOVIGN EQUATION[J]. CHINESE JOURNAL OF COMPUTATIONAL PHYSICS, 1992, 9(S2): 810-811.
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http://www.cjcp.org.cn/EN/Y1992/V9/IS2/810
