搜索资源列表
RKF78FlowRKF7(8)
- 用于卫星轨道动力学计算的R-g数值算法,该算法简单但精度高,易于程序实现,希望对大家有帮助-to calculate the orbit of a satellite in dynamic motherd,this code is easy to understand and use,I hope it will be helpfull for you!
spaceborne_SAR
- 1.本程序是自己刚刚接触SAR时编写的时域星载SAR点目标回波仿真,包含了卫星轨道模型、计算星目斜距时用到的各种坐标系转换、SAR回波计算模型以及简单的SAR成像模型,希望对初学者有所帮助。 2.相应的参考资料可查找《卫星轨道姿态动力学与控制》及《魏钟铨_合成孔径雷达卫星》;-1. This program is just contact with their own prepared when the time domain SAR spaceborne SAR point target
ELCORD.14
- 轨道计算,主要应用于美国空间中心公布的双行根数计算。进行预报。-Orbital calculations, mainly used in the U.S. Space Center announced the number of double-root calculation. To predict.
kalman-filter
- Kalman滤波器在各个领域都有广泛的应用, 如航天器的轨道计算、雷达目标跟踪、生产过程的自动控制等. 卡尔曼滤波器在机动目标跟踪中具有良好的性能, 它是一种最佳估计并能够进行递推计算.-kalman filter
the-stability-of-railway-track
- 铁路轨道稳定性计算程序,用于铁路轨道的设计过程中的稳定性验算-the stability of railway track
SxP4Test
- SGP4轨道计算源码 C++程序,Norad-SGP4 orbit calculation code C++ NORAD SGP4/SDP4 Implementation
orbit
- 轨道计算方法和一些学习资料,非常有用,初学者有用-orbit method
TLE
- 极轨卫星轨道计算模型,用于从两行参数文件中提出信息并计算卫星运行轨道参数.-hda kleqwo ffwefj asdasld ladq dasdakd qweiqw
cppOrbitTools-test
- 轨道计算,根据TlE轨道参数计算出ECI坐标等空间物体信息。-orbit computing
coe_from_sv
- 有卫星状态向量转移至轨道根数,在轨道计算中很常用。-The transfer of the satellite state vector to the orbital elements is very commonly used in orbital calculations.
KSolveKeplerEe
- 开普勒方程求解函数, 方便简单,,空间飞行器轨道计算常用 -Kepler equation solver function, convenient and simple, commonly used in space vehicle orbital calculations
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
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 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
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.