Long-term stability of horseshoe orbits

被引:38
作者
Cuk, Matija [1 ]
Hamilton, Douglas P. [2 ]
Holman, Matthew J. [3 ]
机构
[1] SETI Inst, Carl Sagan Ctr, Mountain View, CA 94043 USA
[2] Univ Maryland, Dept Astron, College Pk, MD 20742 USA
[3] Smithsonian Astrophys Observ, Cambridge, MA 02138 USA
关键词
methods: numerical; celestial mechanics; Earth; planets and satellites: dynamical evolution and stability; planets and satellites: individual: Venus; LATE HEAVY BOMBARDMENT; SOLAR-SYSTEM; TROJANS; SATELLITES; EXISTENCE; DYNAMICS; PLANETS; TADPOLE; SATURN;
D O I
10.1111/j.1365-2966.2012.21964.x
中图分类号
P1 [天文学];
学科分类号
0704 ;
摘要
Unlike Trojans, horseshoe co-orbitals are not generally considered to be long-term stable. As the lifetime of Earth's and Venus's horseshoe co-orbitals is expected to be about a Gyr, we investigated the possible contribution of late-escaping inner planet co-orbitals to the lunar Late Heavy Bombardment. Contrary to analytical estimates, we do not find many horseshoe objects escaping after the first 100?Myr. In order to understand this behaviour, we ran a second set of simulations featuring idealized planets on circular orbits with a range of masses. We find that horseshoe co-orbitals are generally long lived (and potentially stable) for systems with primary-to-secondary mass ratios larger than about 1200. This is consistent with the results of Laughlin & Chambers for equal-mass pairs of co-orbital planets and the instability of Jupiter's horseshoe companions. Horseshoe orbits at smaller mass ratios are unstable because they must approach within 5 Hill radii of the secondary. In contrast, tadpole orbits are more robust and can remain stable even when approaching within 4 Hill radii of the secondary.
引用
收藏
页码:3051 / 3056
页数:6
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