搜索资源列表
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)
Earth_orbit_model-master
- 输入年代，选择模式，输出历史时期地球轨道参数与辐射纬度时间分布图(Input time, selection model, output time history earth orbit parameter and radiation latitude time distribution map)
satellite_orbit
- 根据卫星的轨道跟参数计算中低轨道卫星的轨道(calculate the orbit of LEO or MEO satellite)
Example[1]_simpleproblem
- 轨道计算程序包含各个摄动力的表示同时包含雅克比矩阵计算(orbit maneuver yaconbi matrix,derive_jacobian_hessian_jacobian_boundary_left_jacobian_boundary_right_)
orbit
- 给定一组初位置和初速度即可算得卫星运行轨道根数，并转换为惯性坐标系下的三维轨道显示，同时做出了二者机械能和动量矩的比较。(Given a set of initial positions and initial velocities, we can get the number of satellite orbit and transform it into 3D orbit display under inertial coordinate system. Meanwhile, we comp
GPS卫星位置的计算
- 通过对卫星的数据来进行网络编程，利用相关的插值算法实现相关的功能。(The network programming is carried out by the data of the satellite, and the related functions are realized by the relevant interpolation algorithm.)