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guidao
- 卫星在已知轨道六根数的情况下，需要求得其位置速度时的转换软件，非常方便。是基于兰波特方法计算的
matlab
- 轨道六根数的MATLAB程序,轨道六根数的MATLAB程序
matlab
- 轨道六根数的MATLAB程序,轨道六根数的MATLAB程序-6 tracks the number of MATLAB procedures, track the number of six MATLAB program
weixinguidaoliugenshu
- 卫星轨道六根数，基本公式和基本理论-Satellite orbit six numbers, the basic formula and basic theory. . . . . . . . .
MATlAB-gauss
- 已知赤经赤纬计算轨道六根数，采用高斯算法-calculate orbit elements（gauss)
liuguidaogenshu
- 卫星轨道六个根数轨道离心率，半长轴等等的计算。-Root of the number of satellite orbit six orbital eccentricity, semi-major axis, and so calculations.
guidao
- 只需要有轨道的位置矢量和速度矢量，就可以计算轨道六根数-calculate guidao six genshu
satellite_formatin_control
- 通过matlab的simulink中的s函数，对卫星的轨道六根数进行控制，实现卫星编队的队形保持。-By the simulink in matlab s function to track the number of six satellites is controlled to achieve the formation holding satellite formation.
orbital_elements_compute_the_randv
- 该程序可实现由卫星的轨道六根数计算卫星某一时刻对应的速度和位置。并且实现了计算一段时间后（程序中给出的是45min）卫星的速度和位置。-The program can be realized at a time corresponding to the calculated satellite velocity and position by the track number six satellites. And realized a
Compute_and_Verify_the_drift_rate
- 该程序可以实现卫星在地球摄动力的作用下计算卫星轨道六根数随时间的变化情况。-The program can be implemented in the satellite in the role of the earth to calculate the satellite orbit six time of the change.
randv_2_the_six_orbital_elements
- 该程序可以实现已知卫星在地心坐标系下某一时刻的速度和位置，计算卫星的轨道六根数。-The program can realize the speed and position of the satellite in the center of the earth, and calculate the number of the satellite s orbit six.
tracking
- 卫星轨道三维模拟MATLAB代码，应用卫星六根数，四阶龙哥库塔法求解-3D orbit of satellite，MATLAB，
GetSatPos
- 根据 广播的卫星星历六个轨道根数解算卫星的瞬时位置- satID-> Satellite PRN eph_epoch-> Pointer to the proper ephemerides paragraph receipt_time-> Time when the signal reached the receiver transit_time-&g
rv_transfoamation
- 卫星轨道速度位置与轨道六根数转化，考虑了圆轨道的特殊情况-Satellite orbit speed position and track six number conversion, taking into account the special situation of circular orbit
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)
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)
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.)