搜索资源列表
matlab-toolbox-download
- matlab编写的轨道坐标系变换程序 地心直角坐标系与轨道参数互换-Matlab prepare the track coordinates transform procedures geocentric Cartesian coordinate system with the orbital parameters swap
C_newtyle
- 航天工程用轨道卡尔曼滤波器，姿态确定传感器组合为轨道罗盘+磁强计，是当前组合中最为常见的，适合于小型卫星-Kalman filter with orbital spaceflight, the orbital attitude determination sensor combination compass+ magnetometers, is currently the most common combination is suitable for small satellites
20090826_kepler_solver
- 给出了采用牛顿法解超越方程，求解椭圆轨道及双曲线轨道开普勒方程中的偏近点角的源程序及例子；给出了解普适方程的函数及例子，是研究轨道理论中的重要函数，均基于matlab编程-Gives the solution of transcendental equation using Newton' s method, for solving elliptic orbit and the hyperbolic orbits Kepler equation Eccentric anomaly of t
Orbital_compute
- 进行航天器轨道运算经常用到的函数，包括坐标转换，经纬度转换，二体运动，轨道要素计算-For spacecraft orbit operations frequently used functions, including coordinate conversion, latitude and longitude conversion, two-body movement, and so calculated orbital elements
weixingdingwei
- 卫星定位轨道计算，VC++6.0编写的程序，卫星定位轨道计算-GPS orbit calculation, VC++6.0 program written, satellite positioning orbital calculation
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.
Attitude_Kalman_gom
- 卡尔曼滤波器，具体组合为轨道罗盘+磁强计+速率陀螺，具体物理含义请见附件中的注释，航天人可以一目了然-Kalman filter, the specific combination of orbital compass+ magnetometer+ rate gyro, the specific physical meaning, please see attached comments in the space one can at a glance
PA1100headerdecoderSourcCode.r
- PA1100磁头解码芯片源代码。PA1100磁头解码芯片驱动代码，支持银行卡轨道1、2、3数据，支持正反向刷卡，执行结果分别打印出磁条卡的3个轨道数据,The PA1100 head decoder chip source code. PA1100 head decoder chip drive code, support bank card orbital 1,2,3 data support the pros and cons to the credit card, the results
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
Satellite_orbit_design
- 现需要在高度为600~700KM范围内，回归周期为30天的太阳同步轨道上布置一颗L波段的合成孔径雷达卫星。 1. 请设计合适的轨道参数，并仿真对应轨道下一个运行周期内星下点轨迹图（纬度和经度两个图）； 2. 计算多普勒中心频率，多普勒调频率与纬度的关系图（设姿态角为0°，天线视角20°~60°，推荐35°）； 3. 按高斯投影方式，将星下点轨迹图投影到地图坐标上。-Now requires a height of 600 ~ 700KM range, return period
OrbitDynamics
- 卫星轨道动力学的解算，如轨道根数的求解，星历计算等。-Satellite orbital dynamics solver, such as orbital solving
orbit-dynamics2
- 包含了国内外在轨道力学的方面的最新文章，详细介绍了最新研究成果。-Includes domestic and international aspects of orbital mechanics in the latest articles, detailing the latest research results.
orbit-dynamics3
- 包含了国内外在轨道力学的方面的最新文章，详细介绍了最新研究成果及会议文章。-Includes domestic and international aspects of orbital mechanics in the latest articles, detailing the latest research results.
orbit-dynamics4
- 包含了国内外在轨道力学的方面的最新文章，详细介绍了最新研究成果。-Includes domestic and international aspects of orbital mechanics in the latest articles, detailing the latest research results.
orbital-elements
- 卫星轨道参数正反算，根据卫星的位置和速度，求取实时卫星轨道的两行根数，即6个开普勒根数。卫星星历计算以及卫星轨道参数计算-Considered the pros and cons of satellite orbit parameters, depending on the location and speed of the satellite, two lines of strike root of the number of real-time satellite orbit that Ke
quaternclose
- 两个轨道计算的子程序，四元素乘积计算法和空间轨道动力学方程递推的扩展卡尔曼滤波算法。-Calculation subroutine two tracks, the four elements of the product of calculation and orbital dynamics space equation recursive extended Kalman filter algorithm.
Band_Analysis.tar
- The code Band_Analysis can symmetrize the band dispersions calculated using VASP (Vienna Ab-initio Simulation Package), and it also can calculate the projections of each orbital on each atom.
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 -
csOrbitTools
- The OrbitTools Libraries are implementations of NORAD algorithms for determining satellite location and velocity in Earth orbit. The algorithms come from the December, 1980 NORAD document "Space Track Report No. 3". The orbital algorithms