给出了采用牛顿法解超越方程，求解椭圆轨道及双曲线轨道开普勒方程中的偏近点角的源程序及例子；给出了解普适方程的函数及例子，是研究轨道理论中的重要函数，均基于matlab编程-Gives the solution of transcendental equation using Newton' s method, for solving elliptic orbit and the hyperbolic orbits Kepler equation Eccentric anomaly of t

应用matlab求解航天中常用的开普勒方程，简单易懂-Application matlab solving the Kepler equation used in the aerospace

卫星轨道参数正反算，根据卫星的位置和速度，求取实时卫星轨道的两行根数，即6个开普勒根数。卫星星历计算以及卫星轨道参数计算-Considered the pros and cons of satellite orbit parameters, depending on the location and speed of the satellite, two lines of strike root of the number of real-time satellite orbit that Ke