Jumping mechanisms of Trojan asteroids in the planar restricted three- and four-body problems
Jumping mechanisms of Trojan asteroids in the planar restricted three- and four-body problems
复制标题
平面受限三体和四体问题中特洛伊小行星的跳跃机制
DOI:
10.1007/s10569-015-9609-4
复制
发表时间:
2015
影响因子:
1.6
通讯作者:
Kenta Oshima and Tomohiro Yanao
中科院分区:
文献类型:
--
作者:
汪正元;中村正明;桂 法称;Kenta Oshima and Tomohiro Yanao
We explore minimal dynamical mechanisms for the transport of Trojan asteroids between the vicinities of the stable Lagrange pointsandwithin the framework of the planar restricted three- and four-body problems. This transport, called “jumping” of Trojan asteroids, has been observed numerically in the sophisticated Solar System models. However its dynamical mechanisms have not been fully explored yet. The present study shows that invariant manifolds emanating from an unstable periodic orbit around the unstable Lagrange pointmediate the jumping of Trojan asteroids in the Sun–Jupiter planar restricted three-body problem. These invariant manifolds form homoclinic tangles and lobes when projected onto the configuration space through a discrete mapping. Thus the resulted lobe dynamics explains the mechanism for the jumping of Jupiter’s Trojan asteroids. In the Sun–Earth planar restricted three-body problem, on the other hand, invariant manifolds of an unstable periodic orbit arounddo not exhibit clear homoclinic tangles nor lobes, indicating that the jumping is very difficult to occur. It is then shown that the effect of perturbation of Venus is important for the onset of the jumping of Earth’s Trojan asteroids within the framework of the Sun–Earth–Venus planar restricted four-body problem. The results presented here could shed new insights into the transport mechanism as well as trajectory design associated with,, and.