搜索资源列表
test-ghost-simulation
- 利用轨道角动量纠缠态进行双路相关鬼成像，测试性能。-Orbital angular momentum entanglement in a dual ghost imaging, test performance.
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
ISS-change
- 提取两行轨道参数，提取其中的重要航天器轨道信息-Extracting two lines orbital parameters extract the major spacecraft orbit information
orbit
- 卫星轨道的计算，一个小小的卫星轨迹仿真实例-Orbital calculations
adbar2rv
- Matlab M-File to be used in relevant orbital conversions for satellite tracking
ephemeris-two-body
- 通过轨道根数的计算，解算星历二体问题的状态向量-By orbital calculation solver ephemeris two-body problem of the state vector
satellite-numerrical-methods
- 一个卫星轨道动力学建模与仿真的文档，详细介绍了各种数值仿真方法的应用，对搞轨道数值计算仿真的同志很有帮助-A satellite orbital dynamics modeling and simulation of the document, detailing the application of various numerical simulation method to engage in orbit numerical sim
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
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
analemma
- The program computes and plots the equation of time, the declination, and an analemma curve for various orbital parameters. The analemma is the curve traced by the position of the sun, measured at clock noon, over a year
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 paramete
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 t
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 Ea
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.
88276272
- 系统阐述了小天体运动对应的圆型限制性三体问题共线平动点的强不稳定性特征,以及其附 近的条件周期轨道一晕轨道(HaloOrbit)的存在、相应解的构造.这种特殊的轨道形式和共线 平动点附近的弱稳定走廊,可分别用于在深空特殊位置附近定点有各种科学探测目标的探测器和向 节能轨道过渡的通道. - Systematically expounded the small celestial motion corresponding
Matlab_ex2
- 已知ALOS卫星为用户提供的轨道数据并用三维绘图命令画出地球及相应轨道。-Known ALOS satellite orbital data to provide users with three-dimensional drawing commands to draw the Earth and the corresponding track.
tletransform
- 压缩包中自带资源卫星的tle，用matlab读取并绘制半长轴、轨道倾角、偏心率的变化曲线，观察期变化规律，文件读取的技巧很好-Compressed package comes resource satellites tle, using matlab to read and draw the semi-major axis , orbital inclination , eccentricity curve , variation of
sep_ltot
- 航天领域轨道优化电推进轨道转移matlab算法及示例-Aerospace electric propulsion orbital transfer trajectory optimization algorithm and sample matlab