搜索资源列表
GP_Algorithm_luzhenbo
- G-P算法计算关联维的 Matlab 程序 (升级版，mex函数，超快) 作者：陆振波，海军工程大学 欢迎同行来信交流与合作，更多文章与程序下载请访问我的个人主页 电子邮件：luzhenbo@sina.com 个人主页：luzhenbo.88uu.com.cn 更新部分： 引入限制短暂分离参数，使该参数大于序列平均周期时，去除了同一轨道前后点的关联， 使 r 值较小时，ln r - ln C(r) 曲线接近线性 文件夹说明： 1、GP_Alg
sen
- 给出了在卫星轨道确定中的各种测量量及测量噪声，敏感期的测量方程即转换矩阵-given in the satellite orbit determination of measurement and measurement noise, the sensitive phase of the measurement equation that the transformation matrix
卫星轨道计算程序
- 卫星轨道计算程序，内附实测数据与说明文档,Satellite orbit calculation program, containing the measured data and documentation
spaceMatlab.rar
- 航天相关，计算卫星的轨道,是个Kalman滤波算法,space orbit Kalman filtering algorithm,
Matlabtoolbox_space
- Matlab航天器工具箱，用于轨道计算，2D或3D的平面显示，包含计算多卫星轨道动力学模型和地面覆盖分析等-Matlab toolbox spacecraft for orbit calculation, 2D or 3D graphic display, including the calculation of multi-satellite orbital dynamics analysis model and floor coverings
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!
Spacecraft_Control_Toolbox
- The Spacecraft Control Toolbox is composed of MATLAB m-fi les and mat-fi les, organized into a set of modules by subject. It is essentially a library of functions for analyzing spacecraft and missions. There is a substantial set of softwa
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
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
orbit
- Orbit of the satellite using metlab
Satellite-orbit-simulation
- 卫星轨道仿真，源码，C++，定位等信息GEllipticalOrbit.cpp登文件-Satellite orbit simulation
orbit.m
- Displays the orbit of a LEO satellites
orbit
- 基于matlab编程，给定几对初值，利用ode求解奔月的轨道示意图-Matlab-based programming, given a few of the initial value, the use of ODE solving flying to the moon orbit diagram
Orbit-Dynamics-of-Spacecrafts
- 基于MATLAB开发的航天器轨道动力学程序包。-Program package of orbit dynamics of spacecrafts based on MATLAB.
ORBIT-EARTH-TO-MARS
- Determines an orbit earth to mars-Determines an orbit earth to mars
orbit
- 给定一组初位置和初速度即可算得卫星运行轨道根数，并转换为惯性坐标系下的三维轨道显示，同时做出了二者机械能和动量矩的比较。(Given a set of initial positions and initial velocities, we can get the number of satellite orbit and transform it into 3D orbit display under inertial coordinate system. Meanwhile, we comp
orbit
- 编程仿真连续小推力实现GTO到GEO的三阶段转移过程，其中推力器的推力大小为0.8N，轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度，近地点角距为90度。 GTO轨道： ph:185km，ah：35786km，i：28.5°，GEO轨道：h：35786km，i：0°。 卫星质量为6600kg，从GTO到GEO，采用5000s的推力器。取地球半径为6378km，g取值为9.8m/s^2(The three stage transfer process from GTO to G
实验代码
- 卫星姿态控制仿真，包括卫星轨道建模、卫星运动学、动力学建模，跟踪律计算(Satellite attitude control simulation, including satellite orbit modeling, satellite kinematics, dynamic modeling, tracking law calculation)
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)