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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 parameters of the algorithm for the sa
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
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 circular restricted three-bod
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 the observation period , file
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
monitor
- The Monte Carlo Investigation of Trajectory Operations and Requirements (MONITOR) program was developed to perform spacecraft mission maneuver simulations for geosynchronous, single maneuver, and comet encounter type trajectories. MONITOR is a multif
glonass
- The subsystem of spacecrafts of GLONASS system consists of 24 satellites which are in circular orbits 19100 km high, an inclination 64,8 ° and a cycle time of 11 hours 15 minutes in three orbital planes. The orbital planes are carried on longitude on
orbit-maneuver
- 轨道机动源码：各个类比较规范，便于二次开发-Orbital maneuvering Source: each class fairly standard for secondary development
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
liuguidaogenshu
- 卫星轨道六个根数轨道离心率，半长轴等等的计算。-Root of the number of satellite orbit six orbital eccentricity, semi-major axis, and so calculations.
enalem
- 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.
M-Files-for-Orbital-Mechanics
- 轨道设计是飞行器设计专业一门非常重要的专业课。该书是轨道设计的一本经典之作。-Aircraft design professional track design is a very important professional course. The book is designed to track a classic.
el2rv_moon
- 经典算探测器在月球探测器轨道绕行时的位置，以及在该位置时的速度-this function transform classical orbital elements to position and velocity
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.