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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)
coe_from_rv1
- % 此函数由初始轨道的位置和速度矢量轨道参数 % %参考资料: % Howard D.Curtis 《Obital Mechanics for Engineering Students》 % P158-164 4.4 Orbital elements and the state vector % 参考代码：P606-608 D.8 coe_from_sv.m %常量： % mu -
06_UT 数值
- 使用数值积分法对目标轨道进行估计，并对误差传播进行分析(The numerical integration method is used to estimate the target orbit, and the error propagation is analyzed .)
多空轨道交易系统(源码)y（验证码版）上传
- MT4外汇趋势多空轨道交易系统指标(源码)y（验证码版）(Long and short orbit trading system (source code) y (verification code version))
3d2fc6afef7616be16d14a0bac700f0e
- 可以修改功率谱公式，生成任意一种轨道不平顺时域分析图(The power spectrum formula can be modified to generate an arbitrary track irregularity time domain analysis diagram)
arr6
- 数值模拟轨道不平顺，可以做为轮轨激励施加到轨道和轮轨上，研究轮轨的高频振动(Numerical simulation of track irregularities, can apply for wheel-rail incentive on the rail and wheel/rail, high frequency vibration of the wheel/rail)
4
- 设计一个轨道交通自动售票电路，只接受1，2，5元人民币，每张票价定额5元，并支持找零。要求： （1）用状态机方法设计；(Design an automatic rail transit ticketing circuit, accepting only 1, 2, 5 yuan, 5 yuan per ticket, and support change. Requirements: (1) design with state machine method;)
ATP
- 城市轨道交通防护曲线，可以根据车地通信进行连接(Urban rail protection curve, you can connect to the ground communication)
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
- 模拟一条路线，用GPS卫星导航，得到计算轨道，最后得出误差(To simulate a route, navigate with the GPS satellite, get the calculation track, and finally get the error.)
orbit
- 编程仿真连续小推力实现GTO到GEO的三阶段转移过程，其中推力器的推力大小为0.8N，轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度，近地点角距为90度。 GTO轨道： ph:185km，ah：35786km，i：28.5°，GEO轨道：h：35786km，i：0°。 卫星质量为6600kg，从GTO到GEO，采用5000s的推力器。取地球半径为6378km，g取值为9.8m/s^2(The three stage transfer process from GTO to G
Track plate heat dissipation
- 基于气象资料的无砟轨道瞬态温度场特性研究，与实验结果对比一致，可以直接运行(The study of transient temperature field of ballastless track based on meteorological data is consistent with experimental results and can be operated directly.)
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)
MATLAB
- 根据已经给出的半径、速度向量，预测卫星两天后在轨道上面的位置。(Prediction of satellite orbit position according to radius and velocity vecto)
guidao
- 根据给出的速度与位置向量，预测两天后卫星在轨道上面的位置。(According to the velocity and position vector given, the position of the satellite on the orbit is predicted two days later.)
多空轨道交易系统
- 这是一个通道指标的源码 中间是多空线 上下两条轨道是通道线 k线实体突破上轨做多，跌破下轨做空。上下轨分别也是止损位(his is a source of intermediate channel index is two tracks long and short line is the channel line K-line entity breakthrough track, below the short track. The upper and lower rails are also
fuzhiban
- 浮置板轨道的振动特性 对于研究轨道振动有一定的参考价值(The vibration characteristics of the floating plate track have some reference value for the study of the track vibration.)
3halo
- 用matlab进行平动点轨道的绘制，halo轨道绘制，三维曲线(Libration point orbit of halo rendering, 3D curve)