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- 实现地月轨道的模拟以及计算，讨论了卫星有地球到月球的变轨过程。-a discrible of the way to moon
EarthToMars
- 应用matlab语言，应用lambert变轨实现地球到火星的发射窗口的轨道寻优。内涵lambert变轨功能，星历计算等多个函数文件-Application of matlab language, application lambert achieve orbit the Earth to orbit Mars launch window optimization. Connotation lambert orbit function, ephemeris calculations and oth
2
- 案例为运用最有控制原理，实现对火星探测器小推力变轨的控制实现。应用matlab仿真实现-Case for the use of the most control theory, to achieve the low-thrust orbit Mars probe control implementation. Application of matlab simulation
optimization-algorithm
- Ex2_火星探测器小推力变轨，关于优化算法学习-Ex2_ low thrust orbit Mars, learning about the optimization algorithm
二次变轨
- 基于兰伯特问题，应用初值与时间跨度进行轨道六根数计算，也可用于变轨规划设计(Based on Lambert's problem, the initial value and time span are applied to calculate the six numbers of tracks, which can also be used in the planning and design of orbit change.)