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
sgp4Code
- This source code for calculate of element of satellite.
AIAA-2006-6753
- 计算卫星位置用的,源代码,包括很多,比如sgp4模型-Used in calculating the satellite position, the source code, including many, such as model sgp4
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
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#
AIAA-2006-6753
- SGP4官方程序,包括matlab,java,C++等源码和说明文件-Official program of SGP4 model,includes Matlab, VC, Java, etc.
43177432dav-sgp4-Matlab
- sgp4模型matlab代码,大家共同讨论学习(SGP4 model matlab code, people discuss learning together)
cpp
- 这是一个基于SGP4的卫星轨道预测程序,使用test运行,主要模块是sgp4unit(Satellite orbit prediction program based on SGP4)
sgp4算法(卫星轨道计算)
- 根据星历推算卫星轨道。目前网上多数为C编写,這个是Java的。(The satellite orbit is calculated according to the ephemeris. At present, most of the Internet is written by C, and this is Java.)
SGP4
- 精密轨道处理,对集中轨道外推数据的对比以及经度研究(Precision orbit processing, comparison of extrapolated data of centralized orbit and longitude study)
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