搜索资源列表
Astrogator
- STK实现的卫星轨道机动程序，开发环境STK8.1-STK achieve orbit maneuver program development environment STK8.1
EarthToMars
- 应用matlab语言，应用lambert变轨实现地球到火星的发射窗口的轨道寻优。内涵lambert变轨功能，星历计算等多个函数文件-Application of matlab language, application lambert achieve orbit the Earth to orbit Mars launch window optimization. Connotation lambert orbit function, ephemeris calculations and oth
Ephemeris_And_Orbital
- 利用卫星的星历参数计算其轨道，同时还能根据速度和加速度反算星历参数，是基于MFC对话框的编程-Using satellite ephemeris parameters to calculate its orbit, while depending on the speed and acceleration of the inverse ephemeris parameters is based on MFC dialog programming
Solar-panels-day-orientation-program
- 为了解决单自由度太阳帆板在一般倾斜轨道中对日定向的局限性问题，一种常见的方法是让卫星提供辅助的姿态调整。对于对地观测的卫星，一般只要求卫星姿态保持能使有效载荷指向地面，即对卫星的俯仰角和滚转角有限制而对卫星的偏航角没有要求。因此可以调整卫星的偏航角来辅助太阳帆板对日定向。-In order to solve the single degree of freedom solar panels tilted orbits in the general limitations of the probl
huoche
- 火车车厢排序问题 确定缓冲轨道最小数目 缓冲过程-Train carriage track buffer scheduling problems identified during the minimum number of buffer
ALARM
- 城市轨道交通紧急报警与应急管理指挥系统设计方案-city alarm
myradius
- 目标预测，已知距离信息然后预测出飞行器或导弹的轨道，利用ekf预报-object predict
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
Lambert
- 卫星雷曼过度程序，主要用于卫星雷曼过度轨道的计算，程序包括动力学建模、轨道生成等部分-lambert transfer
intelligent-tracing
- 智能小车寻迹程序，实现小车按指定的轨道运行，可行性强，性能稳定-it can realise intelligent tracing and make the car walk in the designed channel
weixingdingwei
- 作者在学习《航天系统》时，在c++6.0环境中实现的卫星定位的算法程序。包括通过轨道根数求卫星状态参数的算法和通过卫星状态参数反求卫星星历的算法。-Author of the study "space system" is in c++6.0 environment to achieve the satellite positioning algorithm. Including through the orbital parameters of the algorithm for the sa
简单智能车VHDL实现
- FPGA实现智能车利用红外传感器使小车沿预定轨道平稳行驶，数码管显示障碍物与小车的距离，距离低于某值则停止运行
Ctrl32
- 实现列表视图，树形视图，轨道条，进度条以及旋转按钮和组合框和编辑框的显示与简单应用。-Achieve a list view, tree view, track bar, progress bar and rotating buttons and combo boxes and edit boxes display and simple application.
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
cpp
- 使用SGP模型进行轨道计算的C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 coordina
cppOrbitTools
- 封装成类的SGP4 SDP4轨道外推算法 考虑的扰动较多 C++版本-The OrbitTools Libraries NORAD SGP4/SDP4 Implementations in C++
csOrbitTools
- 利用两行星历数据，使用SGP4 SDP4外推模型进行轨道计算-The OrbitTools Libraries NORAD SGP4/SDP4 Implementations in C#
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.