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Orbit.rar
- 卫星轨道机动仿真程序。包括轨道机动仿真、初轨计算、开普勒参数和PV值之间的转换等。,orbit mechanics
fortran
- 卫星轨道预测模型SGP的matlab源代码，经过了验证，可行！-SGP satellite orbit prediction model of the matlab source code, after verification, viable!
SATELLITEORBIT
- This paper discusses the establishment and relevant accomplishments of a simple facility used for students learning aids based on the Keplerian Orbit parameters. Three major areas in Orbital Mechanics are discussed in this paper, Orbit of a satel
samer
- very good program in orbit mechanics - very good program in orbit mechanics
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.
My_Orbital_Library
- 非常好的轨道力学程序包，没事可以试一试，反正不花钱。-orbit mechanics package.. good for learning..just try it.
radar
- 航天器轨道力学 ECEF 地心地固系、东北天坐标系、ECI坐标转换 时间基准换算 轨道参数计算-Spacecraft orbital mechanics to EarthFixed ECEF system, northeast sky coordinates, ECI coordinate conversion parameter calculation time base conversion orbit
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 -
Orbital_Mechanics_for_Engineering Student
- 这是用来计算儒略日，坐标转换，轨道设计等的matlab代码，适配于轨道力学课后代码示例(This is used to calculate the Julian day, coordinate conversion, orbit design matlab code, suitable for orbital mechanics after code example)
orbital mechanics
- Orbit mechanics for enginnering students
Matlab程序
- This is a simulation code of orbital mechanics. We simulated the earth's orbit to Mars, and caught the gravity of Venus once, and achieved good results.
TwoBody
- 二体问题求解程序 包含两个文件： 1.orbit_solver.m 初始化程序，数值计算并画图输出。 在此设置卫星的初始位置坐标r0和速度v0，设置仿真起止时间t0和tf，然后可以直接运行即可。 2.dif_orbit_dynamic.m 轨道动力学函数，包括无摄动力学和J2摄动下的动力学方程，具体采取何种动力学需要在此程序中进行设置。(Two body problem solving program There are two files: 1.orbit_ Solver. M initial