three body problem的例句大全

The low-energy lunar landing trajectory design using the invariant manifolds of restricted three body problem is studied.

研究了基于三体问题的不变流形设计低成本登月轨道的问题。

The evidence of correction to the existent motive equations with variable mass in restricted three body problem

对现有的具有变质量的限制性三体问题运动方程予以修正的证明

Escaping trajectories are investigated using a Poincar é map method in the circular restricted three body problem consisting of spacecraft, planet and moon.

基于由飞行器、行星及其卫星组成圆型限制性三体问题模型，通过庞加莱映射的方法，研究了飞行器从行星卫星附近逃逸的问题。

Based on the model of circular restricted three body problem, nominal orbit in a linearized model can be approached by prediction-correction method, and the orbital control strategy is relatively simpler and can be easily realized.

以圆型限制性三体问题作为基本模型，采用预估-校正法逼近线性化模型下的目标轨道，给出在轨运行期间的轨控策略亦是可取的，这种控制措施相对而言较简单，容易实现。

A issues about the orbital modeling of three bodies which are based on ideal rigid body. And therefore give rise to a integrate numerical method of three body problem. The gravity convergence of rigid body is studied based on rigid body model too.

本文讨论了基于理想模型三体轨道运动规律问题，并给出了一个完整的三体问题的数值解决方案；另外还研究了与引力有关的基于刚体模型的天体表面引力收敛问题。

Under the general Circular Restricted Three Body Problem ( CRTBP) model for deep space exploration, the Chief-Deputy spacecrafts formation model was built up.

针对深空探测中具有一般性的圆形限制性三体（CRTBP）模型，进行主从飞行器编队建模。

Hyperspherical harmonic method and its application to three body problem

超球谐函数方法及其在核三体问题中的应用

In this paper, the nonlinear diffraction problem is studied with potential flow theory in frequency domain for three-dimensional floating body sailing in waves on deep water. This problem includes nonlinear diffraction problem and nonlinear wave making problem.

本文应用势流理论和频域方法研究了三维浮体在深水域波浪中航行时的非线性绕射问题，该问题包括非线性兴波问题和非线性绕射问题。

Based on the detailed discussions on a simplified ideal resonant model with perturbations which corresponds to the elliptic restricted three& body problem, we put forward a discriminating method on stability of orbital resonant states by means of an energy relation in this paper.

本文通过对一种简化的椭圆型限制性三体问题对应的受摄理想共振模型的详细讨论，建立了一种用能量关系来判别轨道共振态稳定性的方法。

For the two-dimensional problem, it can generate triangular element meshes and quadrilateral element mesh; for the three-dimensional problem, it can provide a grid cell including the tetrahedron, hexahedron, pyramid, wedge-shaped body and hybrid grids.

对于二维问题，可生成三角形单元网格和四边形单元网格；对于三维问题，提供的网格单元包括四面体、六面体、棱锥、楔形体及杂交网格等。

Inertial navigation is essentially to solve the kinematic problem of a three-dimensional rigid body.

惯性导航本质上要解决的是一个三维空间的刚体运动学问题。