搜索资源列表
SxP4Test
- SGP4和SDP4的vc源代码 可以使用，用来卫星位置计算和计算地面俯仰角-SGP4 and SDP4 of vc source code can be used to calculate the location of satellites and calculate the ground pitch angle
dav-sgp4-Matlab
- 由david vallado更新的轨道确定的程序代码，本程序融合sgp4和sdp4，包含193个文档-this procedure is the sgp4 prediction model from space command. this is an updated and combined version of sgp4 and sdp4
dundee_sgp4
- Example of the fixed (AFSPC compatible) SGP4/SDP4 orbit propagator. (c) Paul Crawford & Andrew Brooks 1994-2010-The resulting diff.txt file should show virtually zero errors if the build worked OK, and the compvec program can be used to com
SxP4Test
- SGP4轨道计算源码 C++程序，Norad-SGP4 orbit calculation code C++ NORAD SGP4/SDP4 Implementation
cppOrbitTools
- 轨道计算小程序，封装多个预报模型，包括SGP4/SDP4模型，同时附一个例子代码-Orbital calculation program package multiple forecasting model, including SGP4/SDP4 model, while attached to an example of code
csOrbitTools
- sgp4/sdp4轨道模拟C#程序 很有用的啊！源码解释！-sgp4/sdp4 orbit simulate
matlab
- 使用SGP模型进行轨道计算的matlab源码 使用两行星历TLE-Simplified perturbations models are a set of five mathematical models (SGP, SGP4, SDP4, SGP8 and SDP8) used to calculate orbital state vectors of satellites and space debris relative to the Earth-centered inertial coo
cpp
- 使用SGP模型进行轨道计算的C源码 使用两行星历TLE-Simplified perturbations models are a set of five mathematical models (SGP, SGP4, SDP4, SGP8 and SDP8) used to calculate orbital state vectors of satellites and space debris relative to the Earth-centered inertial coordina
cppOrbitTools
- 封装成类的SGP4 SDP4轨道外推算法 考虑的扰动较多 C++版本-The OrbitTools Libraries NORAD SGP4/SDP4 Implementations in C++
csOrbitTools
- 利用两行星历数据，使用SGP4 SDP4外推模型进行轨道计算-The OrbitTools Libraries NORAD SGP4/SDP4 Implementations in C#
norad
- TLE 卫星的双行轨道根数SGP/SGP4/SGP8/SDP4/SDP8模型函数及测试运行-Two Line Element
csOrbitTools
- The OrbitTools Libraries are implementations of NORAD algorithms for determining satellite location and velocity in Earth orbit. The algorithms come from the December, 1980 NORAD document "Space Track Report No. 3". The orbital algorithms
mat
- 利用SGP4模型读取TLE根数，并对卫星轨道进行预测(Using SGP4 / SDP4 model, the tle data, that is, the number of track elements in two lines, is read and the track is predicted.)
SGP8_1.0
- SGP是第一个轨道传播器。它是由希尔顿和库尔曼于1966年开发的，这要归功于Kozai在1959年所做的一项研究工作。它是为绕地球轨道运行的卫星制造的，其中包括轨道周期小于225分钟的卫星。该模型假定偏心率低，并且近地点的高度恒定。 SGP4由肯·克兰福德（Ken Cranford）于1970年开发。它是对之前的传播器的改进，目的是跟踪此时轨道上不断增长的卫星数量。它也用于近地卫星。 SGP8也用于近地卫星，几乎类似于SGP4传播器，但计算方法不同。但是，对于大气和重力效应，它遵循相同的模型
for
- 利用SGP4/SDP4模型，读取TLE数据，即两行轨道根数并对轨道进行预测。(Read TLE, number of tracks in two lines, and predict the tracks)