three-body problem

三体问题

Examples

  • In the book scientists attempt to solve the traditional three-body problem in physics in which the otherwise stable gravitational interaction between two objects in space becomes random and unpredictable when a third object is introduced .

    在这本书里，科学家试图揭开物理学中传统的 三体 问题：在宇宙空间中，如果引入第三个物体，两个物体之间稳定的引力作用会变为随机而不可预测。

  • By these judging conditions the effects on the linear stabilities of the triangular libration points in the classic restricted three-body problem with drag are discussed . Some Murray 's results are improved .

    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。

  • Sufficient and Necessary Conditions for the Stability of Equilibrium Points in the Perturbed Circular Restricted Three-Body Problem and Applications

    有摄圆型限制 性 三体 问题平动点稳定的充要条件及应用

  • Estimation on the periods and characteristic exponents of the periodic orbits in the vicinity of the equilibrium points in the restricted three-body problem

    关于 三体 问题平衡点附近周期轨道的周期及特征指数的估计

  • There are plenty of families of periodic orbits surrounding the collinear libration points in Circular Restricted Three-body Problem ( CRTBP ) model .

    圆型限制 性 三体 问题（CRTBP）共线平动点附近存在着大量的周期轨道族。

  • Building Model Using System Identification for Certain Micro Air Vehicle Research on Gravity-Assist Mechanism in Circular Restricted Three-body Problem

    某型微型飞行器验证样机辨识建模研究基于圆型限制 性 三体 模型的借力飞行机理研究

  • Hill curves in the unchanging plane of the general three-body problem

    一般 三体 问题在不变平面上的Hill 零 速度线

  • The ranges of change of the configurations and positions of orbits in general three-body problem

    一般 三体 问题中轨道形状和位置的变化

  • The changes of the argument of periastron and configurations of the orbit in general three-body problem

    一般 三体 问题中轨道的近点方向及形状的变化

  • Research on Gravity-Assist Mechanism in Circular Restricted Three-body Problem

    基于圆型限制 性 三体 模型的借力飞行机理研究

  • The formulas ( 10 ) and ( 11 ) in this paper can be used to discuss the region of motion of the general three-body problem and their concrete results will be discussed in another article .

    文中公式（10）、（11）也可用来讨论一般 三体 问题的运动区域，具体结果将在另文论述。

  • Plane circular restricted three-body problem

    平面圆型限制 性 三体 问题

  • Existence of double star system in circular restricted three-body problem

    圆型限制 性 三体 问题中双恒星系统的存在性

  • Finally the two level differential corrections method was proposed to transform the orbit designed under the circular restricted three-body problem model into the perturbed three-body problem model .

    最后使用两层微分修正方法将圆型限制 性 三体 问题模型下设计的轨道转换到受摄三体问题模型下。

  • Through the analysis of satellite under restrictive three-body problem that considered the gravity of the earth and the moon differential equations of the system are established .

    本文通过分析卫星在地球和月球引力下的限制性 三体 问题，建立了系统的微分方程。

  • A Criterion for The Linear Stability of Eguilibrium Points in the Perturbed Restricted Three-Body Problem and Applications in Robe Problem

    受摄限制 性 三体 问题平动点线性稳定性的判断条件及在Robe问题的应用

  • The effect of an arbitrary external force perturbation upon the stability of equilibrium points in the circular classic restricted three-body problem and the effect of an inertial drag perturbation upon the stabilities of the main equilibrium points in the Robe circular restricted three-body problem are studied by these conditions .

    用所得到的条件，讨论了任意外力摄动对经典圆型限制性 三体 问题三角平动点稳定性的影响和惯性阻力摄动对Robe圆型限制 性三体问题主要平动点的稳定性的影响。

  • The effects of solar gravity perturbation are evaluated as a crucial error of all which based on the Earth-Sun restricted three-body problem and the Sun-Earth-Moon four-body gravitational model .

    主要研究了太阳引力摄动的影响，并基于地-日限制 性 三体 问题和地-日-月四体引力模型分别对太阳引力摄动影响进行了仿真。

  • The Region of Possible Motion of the Planar Circular Restricted Three-Body Problem under the Influence of a Ring

    考虑环影响的平面圆型限制 性 三体 问题的可能运动区域

  • Since the circular restricted three-body problem model ignores the effect of perturbations it can not accurately describe the dynamic characters of the three-body system .

    圆型限制 性 三体 问题模型忽略了摄动因素的影响，在很多情况下不能足够准确地描述三体系统的动力学性质。

  • Model . Experimental Investigation on Resistance of Trimaran Study on Escaping Energy in Circular Restricted Three-body Problem

    基于圆型限制性 三体 问题模型的行星卫星逃逸能量研究

  • The dynamic characters and orbit design strategy of the perturbed three-body problem model was studied .

    本文研究了考虑摄动影响的 三体 问题的动力学性质及其轨道设计。