搜索资源列表
Solution-of-the-orbit-equation
- Solution of the orbit equation: Theta as function of time t. Numerical solution of Kepler’s equation for the elliptical test problem Matlab code-Solution of the orbit equation: Theta as function of time t. Numerical solution of Kepler’s equa
GNSS-Orbit-and
- 卫星轨道钟差卡尔曼修正-国外导航年会ION2011的文章,网络下载需要$25,-Real-time Combination of GNSS Orbit and Clock Correction Streams Using a Kalman Filter Approach
orbit-satellite-navigation
- 完整的空间卫星轨道仿真程序以及空间卫星导航仿真程序。-Complete space orbit satellite navigation and space simulation program and simulation program.
A Tracking Approach for Inclined Orbit Satellites
- An approach to track satellites that are in inclined orbits. Fusion of 2 types of estimators.
Satellite_-orbit-book-source
- satellite orbit随书源码,代码写的非常规范,值得你拥有,-satellite orbit code, deserve your reading.
Chang-E-III-soft-landing-orbit
- 嫦娥三号于2013年12月2日1时30分成功发射,12月6日抵达月球轨道。嫦娥三号在着陆准备轨道上的运行质量为2.4t,其安装在下部的主减速发动机能够产生1500N到7500N的可调节推力,其比冲(即单位质量的推进剂产生的推力)为2940m/s,可以满足调整速度的控制要求。在四周安装有姿态调整发动机,在给定主减速发动机的推力方向后,能够自动通过多个发动机的脉冲组合实现各种姿态的调整控制。嫦娥三号的预定着陆点为19.51W,44.12N,海拔为-2641m(见附件1)。 嫦娥三号在高速飞行的情
Orbit_representation
- Orbit representation
Orbit-Dynamics-of-Spacecrafts
- 基于MATLAB开发的航天器轨道动力学程序包。-Program package of orbit dynamics of spacecrafts based on MATLAB.
orbit
- 计算航天器开普勒轨道方程,并画出其轨道图像-Kepler spacecraft orbit equation to calculate and draw its orbit image
orbit
- MATLAB编写,计算卫星运行轨道,显示星下点轨迹,适用范围较广。-Preparation of MATLAB, the calculation of satellite orbit, display a ground track, wide range of application.
axis-orbit
- 本模型是计算轴心轨迹的理论模型,主要功能是进行轴心轨迹计算。-here is a modle of axis orbit,The main fuction is to calculate axis shaft orbit.
Deep-space-orbit-detection-design
- 深空探测轨道设计方法,为《轨道动力学与控制》大作业源码,可直接运行-Deep space orbit detection design
orbit
- 计算轨道根数,由位置速度计算,a,e,i,Ω,ω,M-orbit number
ORBIT-EARTH-TO-MARS
- Determines an orbit earth to mars-Determines an orbit earth to mars
orbit-design-for-a-TDRS
- 基于STK的低轨飞行器数据中继卫星系统设计结果。-results of system design of TDRS for a low earth orbit vechicle by STK.
orbit
- 这是前几年设计的一个使用华帮(新唐)77E58设计的仿造 ORBIT公司智能高速球机的控制板,里面涉及到曼彻斯特码的编解码原理和软件实践。 可以使用控制器远程控制球机的运动。-This is a few years ago a Chinese help (a fake orbit company intelligent high-speed ball machine control panel of new Tang 77e58) design, which involves to t
npctoty-orbit
- corba技术orbit demo例子 factoty 很好用(Corba technology orbit demo example factoty is in good condition)
Trabalho4
- Simulate the orbit of a satellite in a special effect graphic
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
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