期刊文献+

关于近地小行星轨道演化的初步探索 被引量:4

A PRELIMINARY INVESTIGATION OF THE ORBITAL EVOLUTION OF NEAR-EARTH ASTEROIDS
在线阅读 下载PDF
导出
摘要 本文采用改进的显式辛算法和嵌套的PKF7(8)积分器同时对86颗已命名(或编号)的近地小行星的轨道演化进行了数值研究,在103-104年的时间尺度上,给出了这些小行星轨道演化的状况以及它们与几颗大行星靠近的最小距离,特别是与地球接近的最小距离可小于0.01天文单位,甚至可能比月球还更靠近地球. Both astCroids and comets are small bodies in the solar system, and the near-earthasteroids (NEAs) are a peculiar kind of asteroids. In recent years, the observation andstudy of the NEAs are well developed, and this has become one of the mostimportant fields of the dynamics of the solar system.The NEAs are divided into the following three kindst (1) Atentype with a < 1.0au and Q > 1.0 au, (2) Apollo-type with a > 1.0 au and q < 1.0 au, (3) Amonr-typewith a > 1.0 au and 1.0 au < q < 1.38 au. Here a is orbital semi-major axis, q =a(1 - e) is Perihelion distance, Q = a(1 + e) is aphelic distance, e is orbita eccentricity,au is astronomical unit, and 1.38 au is the perihelion distance of Mars.In order to clarify the orbital evolution of the NEAs, it is necessary to performlong-term tracking computations. Hence the requirement for algorithm is very high.Ths means that the algorithm must maintan the global characteristics of the motions.Furthermore, the motion of a NEA corresponds to a Hamiltonian system. Thus thesymplectic algorithms just satisfy the requirement, because the symplectic differenceschemes preserve exactly the symplectic structure, which is one of the most importantfeatures for Hamiltonian phase flows.Based on the property that the motoons of the NEAs can be described by themodel of a two-body problem with perturbations, we use the composition of algorithmto construct an improved explicit symplectic algorithm with higher effciency. By useof the improved symplectic algorithm, the orbital evolutions of 86 NEAs for a timespan of 103-104 years are computed and some impohant results are presented in thepaper, e.g., (1) The orbits of asteroid #3552 and #4015 are unstable, (2) The minimaldistance between the asteroid #4660 and the Earth is close to 0.0018 au, which is lessthan the mean distallce between the Moon and the Earth.
作者 刘林 季江徽
机构地区 南京大学天文系
出处 《天文学报》 CSCD 北大核心 1997年第4期337-352,共16页 Acta Astronomica Sinica
基金 紫金山天文台小行星基金 国家自然科学基金
关键词 近地小行星 轨道演化 辛算法 最小距离 near-earth asteroid(NEA) orbital evolution symplectic algorithm minimal distance
  • 相关文献

参考文献4

  • 1刘林,紫金山天文台台刊,1997年,16卷
  • 2廖新浩,计算物理,1994年,11卷,212页
  • 3Feng K,J Comput Math,1986年,4卷,279页
  • 4Feng K,Proc 1984 Beijing Symposium on Differential Geometry and Differential Equations

同被引文献15

  • 1廖新浩,刘林.一种改进的显式辛算法[J].计算物理,1994,11(2):212-218. 被引量:5
  • 2廖新浩,刘林.轨道共振特征及其演化[J].紫金山天文台台刊,1989,8(4):229-273. 被引量:1
  • 3刘林,廖新浩.关于数值求解天体运动方程的几个问题[J].天文学报,1997,38(1):75-85. 被引量:6
  • 4CHAPMAN C R. Comet on target for Jupiter[J]. Nature, 1993,363 : 492-493.
  • 5CHAPMAN C R. Preparing for the comet crash[J].Nature,1993,365:784-785.
  • 6SEKANINA Z. Disintegration phenomena expected during collision of comet Shoemaker-Levy 9 with Jupiter [J]. Science, 1993,262 : 382-387.
  • 7WEAVER H A. Hubble space telescope observations of comet P/Shoemaker-Levy 9 (1993e) [J]. Science,1994,263:787-791.
  • 8SCOTTI J V,MELOSH H J. Estimate of the size of comet Shoemaker-Levy 9 from tidal breakup model[J]. Nature, 1993,365 : 733-735.
  • 9ASPKAUG E,BENZ W. Density of comet Shoemak-er-Levy 9 deduced by modelling breakup of the parent" rubble pile [J]. Nature, 1994,370:120-124.
  • 10季江徽,廖新浩,刘林.辛差分格式的守恒量及其稳定性[J].计算物理,1997,14(1):68-74. 被引量:4

引证文献4

二级引证文献8

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部