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 compve
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 t
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 Ea
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&
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
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)