搜索资源列表
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
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
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.
Input-Data
- matlab编写的计算GPS卫星轨道参数的程序，代码很多，希望大家喜欢-matlab prepared compute GPS satellite orbit parameters of the procedure, code a lot, hope you like
satellite-numerrical-methods
- 一个卫星轨道动力学建模与仿真的文档，详细介绍了各种数值仿真方法的应用，对搞轨道数值计算仿真的同志很有帮助-A satellite orbital dynamics modeling and simulation of the document, detailing the application of various numerical simulation method to engage in orbit numerical simulation comrades helpful
GP_Algorithm2.0
- G-P算法计算关联维的 Matlab 程序 (升级版，mex函数，超快) ----------------------------------- 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_Algorithm_main.m - 程序主文件 2、Lo
Satellite_orbit_design
- 现需要在高度为600~700KM范围内，回归周期为30天的太阳同步轨道上布置一颗L波段的合成孔径雷达卫星。 1. 请设计合适的轨道参数，并仿真对应轨道下一个运行周期内星下点轨迹图（纬度和经度两个图）； 2. 计算多普勒中心频率，多普勒调频率与纬度的关系图（设姿态角为0°，天线视角20°~60°，推荐35°）； 3. 按高斯投影方式，将星下点轨迹图投影到地图坐标上。-Now requires a height of 600 ~ 700KM range, return period
EarthToMars
- 应用matlab语言，应用lambert变轨实现地球到火星的发射窗口的轨道寻优。内涵lambert变轨功能，星历计算等多个函数文件-Application of matlab language, application lambert achieve orbit the Earth to orbit Mars launch window optimization. Connotation lambert orbit function, ephemeris calculations and oth
Ephemeris_And_Orbital
- 利用卫星的星历参数计算其轨道，同时还能根据速度和加速度反算星历参数，是基于MFC对话框的编程-Using satellite ephemeris parameters to calculate its orbit, while depending on the speed and acceleration of the inverse ephemeris parameters is based on MFC dialog programming