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Numerical Simulation on Orbital Stability of RKBOs
WU Xiaomei, NIE Qingxiang
CHINESE JOURNAL OF COMPUTATIONAL PHYSICS    2009, 26 (3): 467-474.   DOI: 10.3969/j.issn.1001-246X.2009.03.020
Abstract283)      PDF (419KB)(1203)      
Orbital evolution of RKBOs is simulated by using reliable orbital elements over a timescale of 108 year.It shows that their orbits are relatively stable in resonant regions.Stability depends on initial orbital semi-major axis,eccentricities and inclinations of these resonant bodies.According to dynamical behavior of orbital semi-major axis,eccentricity and inclination,RKBOs are classified into regular or chaotic orbits.
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