搜索资源列表
convert
- 主要包括卫星轨道计算中的时间和坐标系转换，包括日期转成儒略日、直角坐标转成轨道要素等 -Including satellite orbit calculation time and coordinate system conversion, convert the date to Julian Day, Cartesian coordinates turn into orbit elements
sunsnchronous
- 太阳同步卫星及其轨道计算，用于设计太阳同步轨道，并且给出一个实例，介绍卫星轨道参数的计算方法-Sun-synchronous satellites and their orbital calculations for the design of a sun-synchronous orbit, and an example is given, satellite orbit parameters calculation method
matlab_euler
- 航天器轨道计算中的eular方程应用函数。-Spacecraft orbit calculation eular equation application functions.
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
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#
lambertI
- 功能强大的多圈兰伯特轨道转移程序，而且还可以选择顺时针或逆时针轨道转移，本人轨道计算时使用的程序。-Powerful multi-turn Lambert orbit transfer programs, but you can also choose clockwise or counterclockwise orbit transfer, orbital calculation program I use.
quaternclose
- 两个轨道计算的子程序，四元素乘积计算法和空间轨道动力学方程递推的扩展卡尔曼滤波算法。-Calculation subroutine two tracks, the four elements of the product of calculation and orbital dynamics space equation recursive extended Kalman filter algorithm.
shadow
- 计算卫星在太阳阴影下的位置，实用于卫星轨道计算，-calculate the sun shadow of satellite
sgp17src
- SGP4轨道计算算法，基于NOARD两行根数。-SGP4 Orbit Algorithm.
TLE-Data
- 从某网站上下载的部分卫星两行根数，可用于卫星轨道计算和轨道预报。-Satellite TLE data a website , can be used in the satellite orbit and orbit prediction calculation.
sgp4
- 使用Excel制作的基于SGP4模型的卫星轨道计算工具-use Excel calculate that base on SGP4 module to get satellite orbit tool
BasicAerospaceCode
- 包含了基本的航空航天动力学代码，如坐标转换、Lambert轨道计算等。-Contains basic Aerospace dynamics code, such as coordinate conversion, Lambert orbit calculation, etc..
launchvehicle
- 计算轨道 计算轨道 计算轨道 -compute DATA
H1
- 卫星轨道计算 ECI ECEF TOPO 坐标系以及相关输出函数等-satellite orbit
Matlab
- SGP4matlab模型 使用SGP模型进行轨道计算的matlab源码 使用两行星历T-sda sda sdas dsadas
车桥耦合
- 可以计算车桥耦合动力响应，得到不同轨道不平顺下的动力响应(The dynamic response of vehicle bridge coupling can be calculated, and the dynamic responses under different track irregularities are obtained)
Orbit2ECI
- 计算轨道系到坐标系的转移矩阵，对轨道动力学新人有一定帮助(Transfer matrix of orbit system to coordinate system)
orbit_matlab
- 卫星轨道预报相关程序，包含摄动计算及坐标系转换(Satellite orbit prediction program, including perturbation calculation and coordinate system transformation)
wide juncture of CTRS2
- ansys CRTSＩＩ型板式无砟轨道结构建模(Modeling of ANSYS CRTSII slab ballastless track structure)