搜索资源列表
MIN_CURVE_SURF.rar
- 最小曲率法的算法原理,以及算法例子. 有配图说明 最小曲率法是定向井、水平井轨道设计、测斜计算中经常使用的一种方法。在最小曲率法中，假设井段是空间斜平面上圆弧；对于滑动钻进方式，圆弧是非常合理的井眼轨迹曲线。,The MIN_CURVE_SURF function interpolates a regularly- or irregularly-gridded set of points, over either a plane or a sphere, with either a mini
sgp.rar
- NORAD公布的两行星历数据计算轨道参数模型，本程序包括SGP SGP4 模型,NORAD released two calendar data planet orbit-parameter model, the process includes the SGP SGP4 model
CPP.rar
- NORAD公布的两行星历数据计算轨道参数模型，本程序包括SGP SGP4 模型，是用C++写的！前面上传了matlab版本，请读者搜索一下就可以找到,NORAD released two calendar data planet orbit-parameter model, the process includes the SGP SGP4 model is C++ Written! From in front of a matlab version, readers can be found
SolveKeplerEquationforE.rar
- 开普勒方程求解函数, 方便简单，空间飞行器轨道计算常用,Solve Kepler s Equation for E
suanfa
- 用复合辛普森公式计算卫星轨道长度的程序.-Compound Simpson formula satellite orbit length of the procedure.
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.
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
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
David-Vallado
- 通过NOARD的TLE参数进行轨道参数计算，得出ECI坐标等信息。-Through the NOARD TLE parameters of orbit parameters calculated, ECI coordinates and other information.
SAR-satellites
- 利用SAR卫星在多个时刻的位置和速度信息，计算出任意象元成像时刻卫星的位置，拟合出SAR卫星的轨道模型。-Using SAR satellite in multiple time position and velocity information to calculate as the image element imaging time satellite position, fitting the SAR satellite orbital model.
Three_body_question
- 三体问题，用于求解地球、月球的轨道的计算，运用的是龙格库塔法-Three-body problem is used to solve the earth, the calculation of the orbit of the moon, using the Runge-Kutta method
satellite-numerrical-methods
- 一个卫星轨道动力学建模与仿真的文档，详细介绍了各种数值仿真方法的应用，对搞轨道数值计算仿真的同志很有帮助-A satellite orbital dynamics modeling and simulation of the document, detailing the application of various numerical simulation method to engage in orbit numerical simulation comrades helpful
daily-insolation
- 长时间尺度上的不同纬度的日太阳辐射的计算，假设地球在轨道上的运动是匀速的-Calculation day long the sun at different latitudes on the radiation scale, assuming the Earth' s motion in orbit is uniform in
orbital-paraments
- 计算长时间尺度上的地球轨道参数，包括偏心率，地轴倾角和岁差-Earth' s orbital parameters calculation time scales, including the eccentricity, the earth' s axis tilt and precession
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.
two-body
- fortran语言编写的二体问题轨道外推模块，利用4阶经典RK方法计算微分方程组-two-body problem orbit extrapolation module, use 4-order classical RK method to calculate differential equations
fieqei_v32
- 包括轨道机动仿真、初轨计算,算法优化非常好，几乎没有循环，gmcalab 快速广义的形态分量分析。- Including orbital maneuvering simulation, initial orbit calculation, Algorithm optimization is very good, almost no circulation, gmcalab fast generalized form component analysis.
bengmang
- 包括轨道机动仿真、初轨计算,使用拉亚普诺夫指数的公式，混沌的判断指标Lyapunov指数计算。- Including orbital maneuvering simulation, initial orbit calculation, Raya Punuo Fu index using the formula, Chaos indicator for Lyapunov index calculation.
Oribit Design
- 1.基于龙格库塔方法的卫星轨道六要素计算 2.卫星轨道优化(1.Six elements calculation of satellite orbit based on Runge Kutta method 2.Satellite orbit optimization)