translunar

Calculation method of translunar trajectories for direct striking in specified conditions

给定条件下直接命中月球轨道计算方法

The time systems and the coordination systems that refered to the design process of translunar-trajectory were introduced. The simplified model based on the double two-body hypotheses was given.

对月球转移轨道设计过程中涉及到的时间系统和坐标系统进行了介绍；给出了双二体假设下的轨道设计模型；综合考虑各种影响因素，建立了地月转移轨道的完整动力学模型。

An improved model for translunar trajectory calculation is proposed, which can merge lunar status information directly into the analytical model. Calculations and comparisons show that calculation accuracy can be improved without obvious change of model complexity.

提出了一种改进的地月转移轨道计算模型，改进模型将月球状态信息直接融入解析模型中，经计算对比证明在模型复杂度没有明显变化的前提下提高了模型计算精度。

Technology of the Moon Exploration& Orientation Control for Lunar Probe during Translunar Injection

月球探测技术&奔月变轨过程自旋稳定指向控制

In this paper, obtained the translunar trajectory for direct striking the moon, which satisfied some constraints including translunar flight time, lunar landing date.

在给定飞行时间、着月时间、着月入射角及停泊轨道等约束条件下，建立飞月轨道数学模型；

Study of Sorting Algorithm Investigation on Translunar Trajectories for Lunar Impact

排序算法的探讨击中月球的转移轨道研究

Technology of the Moon Exploration& Orientation Control for Lunar Probe during Translunar Injection

月球探测技术&奔月变轨过程自旋稳定指向控制