搜索资源列表
ECEF2OrbitFrame
- convert from earth fixed earth centered coordinate system to orbital frame (of a satellite) coordinate system.
orbitposition
- 轨道根数与位置速度互化,对于初学轨道知识的人有一定的用处。-Orbital velocity and position of each of, for beginners who have some knowledge of the track usefulness.
astrogator
- 属于stk二次开发，通过matlab调用stk中astrogator模块，实现轨道转移-Belonging to the stk secondary development, matlab call stk in the astrogator module, orbital transfer
coe_from_sv
- 将状态矢量转换成轨道根数的Matlab源程序，输入是位置速度矢量，输出是轨道根数，有详细的注解-Convert the state vector of the orbital elements of the Matlab source code, enter the location of the velocity vector, the output of the orbital elements, with detailed comments
main1
- 数学建模中模拟卫星轨道的matlab源程序，由仿真数据模拟卫星轨道方程中的参数，得到轨道方程。-Matlab source, by mathematical modeling to simulate the satellite orbit parameters in the simulation data analog satellite orbit equation, the orbital equation.
adbar2rv
- Matlab M-File to be used in relevant orbital conversions for satellite tracking
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
nengyao
- 包括轨道机动仿真、初轨计算,matlab编写的元胞自动机，采用偏最小二乘法。- Including orbital maneuvering simulation, initial orbit calculation, matlab prepared cellular automata, Partial least squares method.
kenqan_v25
- esprit算法对有干扰的信号频率进行估计,包括轨道机动仿真、初轨计算,MIMO OFDM matlab仿真。- esprit algorithm signal frequency interference can be assessed Including orbital maneuvering simulation, initial orbit calculation, MIMO OFDM matlab simulation.
giefen
- 包括轨道机动仿真、初轨计算,插值与拟合的matlab实现，利用最小二乘法进行拟合多元非线性方程。- Including orbital maneuvering simulation, initial orbit calculation, Interpolation and fitting matlab implementation, Multivariate least squares fitting method of nonlinear equations.
lenyao_v36
- 包括轨道机动仿真、初轨计算,插值与拟合的matlab实现，matlab开发工具箱中的支持向量机。- Including orbital maneuvering simulation, initial orbit calculation, Interpolation and fitting matlab implementation, matlab development toolbox support vector machine.
feimeng
- 滤波求和方式实现宽带波束形成，包括轨道机动仿真、初轨计算,matlab开发工具箱中的支持向量机。- Filtering summation way broadband beamforming, Including orbital maneuvering simulation, initial orbit calculation, matlab development toolbox support vector machine.
henqou_v23
- 包括轨道机动仿真、初轨计算,matlab实现了五类灰色关联度模型的计算,多姿态，多角度，有不同光照。- Including orbital maneuvering simulation, initial orbit calculation, matlab implements five gray correlation degree computing model, Much posture, multi-angle, have different light.
taoqan
- 现代信号处理中谱估计在matlab中的使用，针对EMD方法的不足,包括轨道机动仿真、初轨计算。- Modern signal processing used in the spectral estimation in matlab, For lack of EMD, Including orbital maneuvering simulation, initial orbit calculation.
buikan_v56
- 课程设计时编写的matlab程序代码，预报误差法参数辨识-松弛的思想，包括轨道机动仿真、初轨计算。- Course designed to prepare the matlab program code, Prediction Error Method for Parameter Identification- the idea of relaxation, Including orbital maneuvering simulation, initial orbit calculation.
henheng_v83
- 基于小波变换的数字水印算法matlab代码，滤波求和方式实现宽带波束形成，包括轨道机动仿真、初轨计算。- Based on wavelet transform digital watermarking algorithm matlab code, Filtering summation way broadband beamforming, Including orbital maneuvering simulation, initial orbit calculation.
gangyiu
- 用MATLAB实现动态聚类或迭代自组织数据分析，cordic算法的matlab仿真，包括轨道机动仿真、初轨计算。- Using MATLAB dynamic clustering or iterative self-organizing data analysis, cordic matlab simulation algorithm, Including orbital maneuvering simulation, initial orbit calculation.
Orbital_Mechanics_for_Engineering Student
- 这是用来计算儒略日，坐标转换，轨道设计等的matlab代码，适配于轨道力学课后代码示例(This is used to calculate the Julian day, coordinate conversion, orbit design matlab code, suitable for orbital mechanics after code example)
新建文件夹
- 利用matlab对卢瑟福散射进行仿真。但是因为电子质量很小，而且a粒子和电子的碰撞近似为完全弹性碰撞（因为这种碰撞能量很小，不会发生能级间的跃迁），根据动量守恒和能量守恒可以知道，a粒子速度几乎不变，对实验的结果影响很小。电子如果被撞到的话，估计就会被撞飞了吧，也可能被a粒子或者靶中其他失去电子的阳离子俘获.利用平方反比有心力场中的第三运动积分—Runge-Lenz矢量,简化处理了卢瑟福散射、氢原子的量子化和氢原子园轨道的相对论修正问题.(221/5000 Matlab is used t
Matlab程序
- This is a simulation code of orbital mechanics. We simulated the earth's orbit to Mars, and caught the gravity of Venus once, and achieved good results.