搜索资源列表
the-three-laws-of-Keplers
- 可以实现开普勒三定律，只是要输入数据而已-The realization of the three laws of Kepler s
KSolveKeplerEe
- 开普勒方程求解函数, 方便简单，，空间飞行器轨道计算常用 -Kepler equation solver function, convenient and simple, commonly used in space vehicle orbital calculations
orbit
- 计算航天器开普勒轨道方程，并画出其轨道图像-Kepler spacecraft orbit equation to calculate and draw its orbit image
kepler-equaction-DG
- 数值计算方法！利用离散梯度法计算开普勒方程！理论扎实易懂，方便学习-Numerical methods! Kepler equation is calculated using the discrete gradient method! Theory of solid and easy to understand, easy to learn
Two-body-problem
- 二体问题的求解，以读文件的形式输入，解算结果为6个开普勒轨道根数-Two body problem solving, in order to read documents in the form of the input, the calculating results for root number six Kepler orbit
theehe
- 这是用于计算天文中的开普勒轨道元素的程序,用MAtlab编写的,欢迎使用哦,-This is used to calculate the Kepler orbit elements in the astronomical program, using MAtlab, welcome to use oh,
podgram
- 这是用于计算天文中的开普勒轨道元素的程序,用MAtlab编写的,欢迎使用哦,-This is used to calculate the Kepler orbit elements in the astronomical program, using MAtlab, welcome to use oh,
NWVN1
- 这是用于计算天文中的开普勒轨道元素的程序,用MAtlab编写的,欢迎使用哦,(This is used to calculate the Kepler orbit elements in the astronomical program, using MAtlab, welcome to use oh,)
spinning tether
- 基于Mathcad（也可转为matlab程序）的旋转系绳系统模型，以牛顿力学建模，考虑系绳弹性，可用于任意开普勒轨道建模仿真。(The Mathcad based model of the rotating tether system, which considers the tether elasticity, can be used for arbitrary Kepler orbit modeling and simulation.)
1
- 关于航天器航天器轨道力学轨道参数计算，利用开普勒定律计算六个轨道根数等(The orbit parameters of spacecraft, ft and spacecraft are calculated)