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taiyangxixingxingguijijiyunxing
- 用vb6.0编写的一个太阳系行星轨道及运行 3D立体动画演示程序。 -Prepared using vb6.0 and run a planets orbit stereo 3D animation program.
OrbitDynamics
- 这是我在CSDN上找到的比较好的一个关于卫星轨道动力学的一个源码包，简单易懂，用c++写的，作者是韩冬，向他致敬！ 非常好用的程序，学习卫星轨道动力学-This is I find in good CSDN about the dynamics of the satellite s orbit a source packages, easy to understand and use c++ written, the writer is HanDong, paid tribute to hi
Hohmann
- 典型的霍曼变轨算法，简单易懂，有清晰的注释-Hohmann orbit typical algorithm, easy to understand, there is a clear Notes
gpredict-1.3
- Gpredict is a real-time satellite tracking and orbit prediction application. It can track an unlimited number of satellites and display their position and other data in lists, tables, maps, and polar plots (radar view). Gpredict can also predict the
PassFinder
- 全球卫星轨道预测模型SGP4的一个实现，采用java开发，提供学习的源码。-Global satellite orbit prediction system, java development, to provide source code.
GPS-satellite-track
- 以GPS卫星为例，主要介绍利用SDP8模型，预报GPS卫星在几天内的星历，从而利用BorlandC++Builder 编程实现GPS卫星星座、星下点轨迹仿真及全球DOP值图形分析，测站星空图变化，测站DOP值分析，从而更好的分析GPS卫星星座、轨道变化、卫星的性能, 为改进卫星的星座及轨道提供技术依据。-This paper introduces that is using SDP8 propagation model to predict GPS of position and velocit
Tracking--Inclined-Orbit-Satellites
- Algorithm for tracking inclined orbit satellites
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
huiguiguidao
- 回归轨道卫星，回归周期1天，倾角分别为60度，周期为4h。-Orbit satellites, one day return period, inclination of 60 degrees and a period of 4h.
diqiujingzhiguidao
- 1.地球同步轨道卫星，倾角分别为0，30，90度。 -1 satellites in geosynchronous orbit, respectively 0,30,90 degrees inclination.
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
Application
- 星历计算，通过两个观测历元来计算卫星的轨道参数-Ephemeris calculations by two epoch observations to calculate the satellite orbit parameters
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
LOIC-1.0.8-binary
- Low Orbit Ion Cannon (LOIC) is an open source network stress testing and denial-of-service attack application, written in C#. LOIC was initially developed by Praetox Technologies, but was later released into the public domain, and now is hosted on se
sgp17src
- SGP4轨道计算算法，基于NOARD两行根数。-SGP4 Orbit Algorithm.
guangboxingli
- 广播星历进行卫星定轨，使用C#语言，精度1-2米，适合卫星定位相关服务或者研究GPS初学者研究使用-Broadcast ephemeris satellite orbit determination using the C# language, accuracy of 1-2 meters, for satellite positioning services or research studies using GPS for beginners
C-W
- 使用CW方程，使用最小能量，采用脉冲推力，实现在一天内两航天器的交会对接。本质上就是一个交会轨道优化问题，由给定的条件优化选取设计变量，使目标函数得到最优值。-Using the CW equation, use the minimum energy, the use of pulse thrust, to achieve in a day two spacecraft rendezvous and docking. Is essentially an intersection orbit op