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1.
舒斯会  陆本魁 《天文学报》2005,46(2):165-172
研究了Coriolis力和离心力摄动对Robe限制性三体问题主要平动点位置及线性稳定性的影响,给出了Robe限制性三体问题主要平动点的摄动位置和Coriolis力和离心力摄动对主要平动点位置和线性稳定的影响量级.改进了Shrivastava的结果.  相似文献   

2.
给出了受摄限制性三体问题平动点线性稳定性的一个判断条件.条件只与平动点切映像的特征方程系数有关,使用方便.用判断条件,讨论了Robe问题平动点在阻力摄动下的线性稳定性,得到了Hallan等给出的Robe问题平动点在阻力摄动下的线性稳定范围.并改进了Giordanoc等的结果.  相似文献   

3.
给出了受摄限制性三体问题平动点线性稳定性的一些判断条件,条件只与相应的平动点切映像的特征方程系数有关,使用方便,用这些判断条件,讨论了一些阻力对经典限制性三体问题三角平动点线性稳定性的影响,改进了Murray等的一些结果。  相似文献   

4.
Lagrange三角平动邻近的相空间结构   总被引:1,自引:0,他引:1  
周礼勇  孙义燧 《天文学报》1999,40(3):286-293
构造描述一类特殊平面圆型限制性三体问题的一个映射,并用这个映射讨论了类三体问题Lagrange三角平动点领近的相空间结构以及它的稳定性,发现当两个主天体的质量比μ〈0.02165时,除去μ=0.01440的例外情况,三角平动点被不变曲线包围,是稳定的。  相似文献   

5.
构造描述一类特殊平面圆型限制性三体问题的一个映射,并用这个映射讨论了该类三体问题Lagrange 三角平动点邻近的相空间结构以及它的稳定性,发现当两个主天体的质量比μ< 0 .02165 时,除去μ= 0 .01440 的例外情况,三角平动点被不变曲线包围,是稳定的,这与理论结果相符,由此可解释特罗央群和希腊群小行星的稳定存在.该结果也验证了映射方法的可靠性和有效性  相似文献   

6.
关于共线平动点的特征及其在深空探测中的应用   总被引:3,自引:0,他引:3  
系统阐述了小天体运动对应的圆型限制性三体问题共线平动点的强不稳定性特征,以及其附近的条件周期轨道——晕轨道(Halo Orbit)的存在、相应解的构造。这种特殊的轨道形式和共线平动点附近的弱稳定走廊,可分别用于在深空特殊位置附近定点有各种科学探测目标的探测器和向节能轨道过渡的通道。  相似文献   

7.
与共线平动点不同,圆型限制性三体问题中的两个三角平动点在一定条件下,无论是线性意义下还是非线性意义下,都是稳定的,其附近存在着周期与拟周期轨道,在深空探测中有应用前景.该文首先简单介绍三角平动点附近运动的动力学特征,然后以日-(地+月)系和地-月系两个三体系统为例,进一步阐述真实引力模型下三角平动点附近的运动状态,最后以这两个三体系统为例,探讨了三角平动点探测器的发射和定点轨道控制问题.  相似文献   

8.
本文研究的是某一考虑主星体形状的椭圆型限制性三体问题。通过这种力学体系的不变关系式,模仿圆型问题的定性方法,并结合摄动方法,讨论了小天体在考虑形状的主星体附近运动时的Hill稳定性问题;特别探讨了本文力学体系的Hill稳定性和圆型问题Hill稳定性之差异。  相似文献   

9.
基于最小二乘法原理的速度因子方法是保流形结构算法中效率最高、稳定性最好、应用最广的方法.利用速度因子方法讨论了主星为辐射源,伴星为扁球的平面圆型限制性三体问题的稳定性问题.数值研究表明:(1)仅考虑扁状摄动项时,系统混沌运动的轨道数量会增多;(2)仅考虑辐射项时,系统有序运动的轨道数量会增多;(3)同时存在辐射和扁状摄动时,辐射占主导作用,系统有序运动的几率会增加.  相似文献   

10.
天文动力学和天体力学   总被引:1,自引:0,他引:1  
叙述了与Astrod工程有关的天体力学和天文动力学的基本结果和学科概况,内容包括二体问题,摄动理论,人造地球卫星运动,限制性三体问题等。  相似文献   

11.
We numerically study a version of the synchronous circular restricted three-body problem, where an infinitesimal mass body is moving under the Newtonian gravitational forces of two massive bodies. The primary body is an oblate spheroid while the secondary is an elongated asteroid of a combination of two equal masses forming a rotating dipole which is synchronous to the rotation of the primaries of the classic circular restricted three-body problem. In this paper, we systematically examine the existence, positions, and linear stability of the equilibrium points for various combinations of the model's parameters. We observe that the perturbing forces have significant effects on the positions and stability of the equilibrium points as well as the regions where the motion of the particle is allowed. The allowed regions of motion as determined by the zero-velocity surface and the corresponding isoenergetic curves as well as the positions of the equilibrium points are given. Finally, we numerically study the binary system Luhman-16 by computing the positions of the equilibria and their stability as well as the allowed regions of motion of the particle. The corresponding families of periodic orbits emanating from the collinear equilibrium points are computed along with their stability properties.  相似文献   

12.
This paper examines the existence and linear stability of equilibrium points in the perturbed Robe’s circular restricted three-body problem under the assumption that the hydrostatic equilibrium figure of the first primary is an oblate spheroid, and the shape of the second primary is also an oblate spheroid. The problem is perturbed in the sense that small perturbations given to the Coriolis and centrifugal forces are being considered. Results of the analysis found two axial equilibrium points on the line joining the centre of both primaries. It is further observed that under certain conditions, points on the circle within the first primary are also equilibrium points. The linear stability of this configuration is examined; it is observed that the first axial point is unstable while the second one is conditionally stable and the circular points are unstable.  相似文献   

13.
This paper examines the existence and stability of the out-of-plane equilibrium points of a third body of infinitesimal mass when the equations of motion are written in the three dimensional form under the set up of the Robe’s circular restricted three-body problem, in which the hydrostatic equilibrium figure of the first primary is an oblate spheroid and the second one is a triaxial rigid body under the full buoyancy force of the fluid. The existence of the out of orbital plane equilibrium points lying on the xz-plane is noticed. These points are however unstable in the linear sense.  相似文献   

14.
This paper considers the restricted circular three-body problem with respect to the radiation repulsion force acting upon a particle on the part of one of the main bodies (the Sun). The characteristic of the family of stationary particular solutions of the problem (libration points) representing the relative equilibrium positions in a rotating Cartesian system is given. On the basis of the KAM theory with the help of a computer a nonlinear analysis of the triangular libration points stability for the planar case is carried out. These libration points are proved to be strictly stable by Liapunov practically in the whole area of fulfilling the necessary stability conditions. Instability is discovered at the resonant curve of the third order and at the greater part of the resonant curve of the fourth order. The plotted results of the investigation allowed us to draw a conclusion about the Liapunov stability of the triangular libration points in a problem with respect to the radiation pressure for all the planets of the Solar system.  相似文献   

15.
The spectral stability of synchronous circular orbits in a rotating conservative force field is treated using a recently developed Hamiltonian method. A complete set of necessary and sufficient conditions for spectral stability is derived in spherical geometry. The resulting theory provides a general unified framework that encompasses a wide class of relative equilibria, including the circular restricted three-body problem and synchronous satellite motion about an aspherical planet. In the latter case we find an interesting class of stable nonequatorial circular orbits. A new and simplified treatment of the stability of the Lagrange points is given for the restricted three-body problem.  相似文献   

16.
The circular restricted three-body problem, where two primaries are taken as heterogeneous oblate spheroid with three layers of different densities and infinitesimal body varies its mass according to the Jeans law, has been studied. The system of equations of motion have been evaluated by using the Jeans law and hence the Jacobi integral has been determined. With the help of system of equations of motion, we have plotted the equilibrium points in different planes (in-plane and out-of planes), zero velocity curves, regions of possible motion, surfaces (zero-velocity surfaces with projections and Poincaré surfaces of section) and the basins of convergence with the variation of mass parameter. Finally, we have examined the stability of the equilibrium points with the help of Meshcherskii space–time inverse transformation of the above said model and revealed that all the equilibrium points are unstable.  相似文献   

17.
This paper examines the existence and linear stability of equilibrium points in the perturbed Robe’s circular restricted three-body problem under the assumption that the hydrostatic equilibrium figure of the first primary is an oblate spheroid. The problem is perturbed in the sense that small perturbations are given to the Coriolis and centrifugal forces are being considered. Results of the analysis found two axial equilibrium points on the line joining the centre of both primaries. It is further observed that under certain conditions, points on the circle within the first primary are also equilibrium points. And a special case where the density of the fluid and that of the infinitesimal mass are equal (D = 0) is discussed. The linear stability of this configuration is examined; it is observed that the first axial point is unstable while the second one is conditionally stable and the circular points are unstable.  相似文献   

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