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卫星轨道坐标的计算方法
- 用VC实现对卫星任意时刻在轨道直角坐标系统和天球坐标系中坐标的计算方法，不同卫星需自行修改其初始状态参数-with VC arbitrary moment of satellites in orbit Cartesian coordinate systems and Celestial Coordinates of the calculation method different satellites take the initiative to revise its initial state
weixing.rar
- matlab实现的卫星轨道模拟，利用卫星轨道根数参量，通过求解开普勒方程求解卫星轨道模型,err
fortran
- 卫星轨道预测模型SGP的matlab源代码，经过了验证，可行！-SGP satellite orbit prediction model of the matlab source code, after verification, viable!
untitled1
- 阿波罗卫星轨道的matlab仿真,可以实现轨道模拟-Apollo satellite orbit simulation
satellite_orbit_improvement6
- 文献：程序覆盖法在卫星轨道改进程序中的应用-Literature: the procedures covered in satellite orbit to improve the application process
trace
- GPS信号模拟器卫星状态参数的算法研究，模拟器，轨道参数，非球形地球引力。-GPS satellite signal simulator state parameters of the algorithm, simulator, orbital parameters, non-spherical Earth' s gravity.
Stratospheric-satellite-orbit-modeling-and-simulat
- 平流层卫星轨道控制建模与仿真Stratospheric satellite orbit modeling and simulation of control-Stratospheric satellite orbit modeling and simulation of control
OrbitalTool
- 分析卫星轨道的MATLAB程序包，很多子程序值得借鉴。-Computing satellite orbit with MATLAB software
308012984
- 开普勒公式卫星轨道模拟 以及 左边转换函数 ECI2ECEF LGCV2ECEF-Simulation of orbital motion by solving Keplerian equation
卫星轨道计算
- 详细介绍了轨道方程，轨道六要素，以及坐标计算方法，包括椭圆轨道面坐标、大地空间直角坐标以及经纬度坐标的计算方法(The orbit equation, the six elements of orbit and the coordinate calculation method are introduced in detail, including the calculation method of elliptical orbit, plane coordinates, geodetic sp
orbit_matlab
- 卫星轨道预报相关程序，包含摄动计算及坐标系转换(Satellite orbit prediction program, including perturbation calculation and coordinate system transformation)
Oribit Design
- 1.基于龙格库塔方法的卫星轨道六要素计算 2.卫星轨道优化(1.Six elements calculation of satellite orbit based on Runge Kutta method 2.Satellite orbit optimization)
gddlx1
- 以x0=[-5292392.072;-4862.201380;3111662.355; -4136.781314;3101114.660； -4147.028008]人造地球轨道卫星的初始条件，编制C或C++程序，计算卫星轨道，并与Matlab的结果进行比较。(The satellite orbit is calculated and compared with the result of Matlab.)
GPS
- 卫星轨道仿真，基于广播星历下的GPS卫星轨道仿真(Satellite orbit simulation)
J2
- 考虑地球扁率摄动，求解近地卫星轨道六根数，(Consider J2 perturbation to solve the number of six tracks)
卫星仿真
- 卫星二体轨道动力学模型仿真，用于卫星轨道模拟，航天领域(Satellite two-body orbit dynamics model simulation)
Satellite Orbit Modeling
- 卫星轨道工具箱，含轨道计算、坐标转换、时间计算等(Satellite Orbit Modeling)
mat
- 利用SGP4模型读取TLE根数，并对卫星轨道进行预测(Using SGP4 / SDP4 model, the tle data, that is, the number of track elements in two lines, is read and the track is predicted.)
卫星轨道根数到位置速度的转换程序
- 卫星轨道常用轨道六要素来描述，通过程序转换，可以得到各个时刻下卫星的位置矢量与速度矢量。
卫星轨道仿真
- simulink卫星轨道仿真，由航天器动力学方程，得到卫星三维位置数据