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train-probles
- 计时功能两列火车同轨道，停止与前进，计算时间速度，选择那一辆停靠，那一辆先行-Timing features two train track, stop and forward, the computation time speed, select that a dock, that a first
satellite-pos
- GPS卫星坐标计算，根据导航卫星星历的轨道参数和摄动改正项来计算卫星的坐标-GPS satellite coordinates to calculate the correction items to calculate the coordinates of the satellite navigation satellite ephemeris orbital parameters and the perturbation
SAR-satellites
- 利用SAR卫星在多个时刻的位置和速度信息，计算出任意象元成像时刻卫星的位置，拟合出SAR卫星的轨道模型。-Using SAR satellite in multiple time position and velocity information to calculate as the image element imaging time satellite position, fitting the SAR satellite orbital model.
Three_body_question
- 三体问题，用于求解地球、月球的轨道的计算，运用的是龙格库塔法-Three-body problem is used to solve the earth, the calculation of the orbit of the moon, using the Runge-Kutta method
Spacecraft-orbit-extrapolation-code
- 航天器轨道外推代码（FORTRAN95/2003科学计算与工程，宋叶志），旨在介绍常微分方程处置问题的应用。-Spacecraft orbit extrapolation code (FORTRAN95/2003 scientific computing and engineering, Sung YE), aims to introduce the ordinary differential equation of the disposal of the application.
Star-a-Planet-Finder
- matlab编写的计算行星位置和轨迹的程序，采用时域并行算法对椭圆轨道进行修正。-Matlab prepared by the procedures of calculating planetary positions and trajectories, using time-domain parallel method for the elliptical orbit correction.
Orbit_compute_state_vector
- 解析法计算二体轨道的Matlab程序，采用f,g量求解-Analytic Calculation of the two bodies orbit in Matlab, using the f and g of solving
calculating-spectrum
- 朔黄重载铁路轨道不平顺谱计算程序,能计算其轨距不平顺谱，并与国内外统计谱进行对比-the calculating programer of Shuohuang Heavy Hual railway of track irregularity,it can calculate the guage irregularity spectrum,and contrast with the foreignal and national statistic spectrum
track-count-and--ephemeris-count
- 运用给出的相关参数，设计一种巧妙计算出轨道参数及反算卫星星历的算法-Use of the given parameters, design an ingenious algorithm calculate the orbital parameters and Inverse satellite ephemeris
GPSweijudingwei
- 对于高轨道的GPS卫星，本程序主要针对伪距的计算测量。-GPS satellites in high orbit, the program is mainly for computing pseudorange measurement.
track_6_elements_compute
- 轨道6根数计算小程序：已知发射点信息，入轨点信息，求取轨道6要素的值。自编小程序-Track six the number of small programs: known launch point information, the orbit point information, the value of the strike track 6 elements. Self applet
EX2
- ALOSPALSAR卫星数据读取及基线计算,利用各种数据插值方法计算数据获取时间内任意时刻的卫星所在的位置,并用三维绘图命令画出地球及相应轨道.-The satellite data read and baseline of ALOSPALSAR interpolation method using a variety of data calculation data for the location of the time at any moment of the satellite, and
erti
- 二体问题是根据牛顿万有引力定律计算卫星轨道位置的计算方法，求取卫星六个轨道参数，应用于导航定位。-wqfrh wqrijqi qwiqd qwjrfhq qajwdqhi quqi sjfo fgiei dfafoif effwe qfefqqnfdqf sofqwofff lfkqq fwpfqkwkq fkqf
calculated-6-orbit-parameter
- 由卫星位置和速度计算出了6个轨道根数，C#编写，运行环境为visual studio,控制台程序-Use satellite position and velocity to calculated 6 orbit parameter, C#, operating environment for the visual studio，Console application
Satellite-ephemeris-calculation-
- 利用瞬时轨道参数计算协议地球坐标系及相关坐标系下的卫星星历，C# 控制台程序。-Satellite ephemeris calculation of earth coordinate system protocol and relative coordinates using instantaneous orbit parameters, a C# console application.
system-phase-portrait
- 用于计算3维4维微分方程的轨道,并根据需要舍去计算中前若干个点-compute the phase portraits of 3D or 4D differatial equations
orbit
- 卫星轨道的计算，一个小小的卫星轨迹仿真实例-Orbital calculations
weixin
- 基于matlab的人造卫星轨道外套计算函数源码-Matlab-based satellite orbit calculation function jacket source
sun
- 用于低轨太阳同步轨道卫星的地影参数的计算-Earth' s shadow calculation
ephemeris-two-body
- 通过轨道根数的计算，解算星历二体问题的状态向量-By orbital calculation solver ephemeris two-body problem of the state vector