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。
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。
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。
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
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
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。
Plane circular restricted three-body problem 平面圆型限制性三体问题
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。
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。
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
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
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 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
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
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 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。
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
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
Some judging conditions for the linear stability of the libration points in the perturbed restricted three-body problem are given. These conditions only depend on the coefficients of the characteristics equations of their tangent maps and are applied expediently. 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。
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
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。
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。
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。