搜索资源列表
DoubleIntegration
- 用于求解二阶常微分方程的变步长多步积分法，适合飞行器轨道计算等领域。-Solving second order ordinary differential equations for the variable step-size multi-step integration method for calculating the fields of aircraft track.
main1
- 这是本科铁道方向课程设计的一个简单的计算程序，用于计算实现轨道“统一公式”-Calculate the formation
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
2012B
- 数学建模，程序编程，在轨道计算中，时间是独立变量。但是，在计算不同的物理量时，却使用不同的时间系统。-Mathematical modeling, programming, orbital calculations, time is the independent variable. However, in the calculation of the different physical quantity, but using different time systems.
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