搜索资源列表
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
matlab.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,matlab implementation of satellite orbit simulation, the number of satellite orbit parameters, by solving the Kepler equation model of satellite orbit
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
GPS
- 计算卫星轨道,包括轨道坐标的计算,此程序为MATLAB样例程序。-Computing satellite orbits, including orbit coordinates calculation, this procedure for the sample MATLAB program.
work
- 本程序用matlab仿真卫星及轨道,希望对大家的学习有所帮助-This procedure simulation using matlab and satellite orbit, and they hope to be helpful to study the U.S.
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.
DrawSatelliteOrbit
- 利用matlab代码绘制卫星轨道,总共包含6个卫星轨道平面-Matlab code to draw the use of satellite orbit, a total of six satellite orbit plane contains
Orbit
- 卫星轨道机动模拟仿真matlab程序,应用GPS数据进行具体分析。-Matlab simulation of satellite orbit maneuver, application specific analysis of GPS data.
sat_orbit
- 这是由Andrea Monti Guarnieri的卫星轨道确定算法,基于的是norad 的tle数据-This is Andrea Monti Guarnieri satellite orbit determination algorithm, is based on the norad of tle data
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
matlab
- 实现卫星轨道控制,知道怎样通过matlab实现卫星的简单模拟-satellite
Matlab-GPS-Toolbox
- 计算GPS卫星轨道数据,包括计算GPS卫星的各个卫星的参数,转化数据等-Calculated GPS satellite orbit data, including the calculation of the various satellite GPS satellite parameters, transforming data, etc.
卫星轨道建模
- 基于matlab的GPS卫星轨道建模与坐标系转化,生成卫星轨道以及卫星在惯性坐标系下的坐标(GPS satellite orbit modeling and coordinate transformation)
卫星轨道模拟程序
- 卫星轨道模拟程序, matlab程序, 有文档说明(satellite orbit simulation matlab code with discr iption)
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.)
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)