搜索资源列表
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!
HMGD_mo_ni
- 理论力学——霍曼轨道运动的matlab计算机模拟 主程序名 hmgd.m 函数名 界面程序名hmgdfun.mhmgdgui-Theoretical Mechanics- Hö rmann computer simulation of orbital motion, matlab main program interface function names were hmgd.m program name hmgdfun.mhmgdgui
Orbital-mechanics-basic-subroutine.RAR
- 轨道力学基本子程序,包括Eular数值积分器、JPL行星精密历表、RKF78阶数值积分器-Orbital mechanics basic routines, including Eular numerical integrator, JPL planetary ephemeris precision, RKF78 order numerical integrator ...
Matlab
- matlab的轨道力学子程序，适用于搞航天航空的专业人士学习和使用。-matlab subroutine of orbital mechanics, for aerospace professionals to engage in learning and use.
Orbit_Mechanics(Matlab)
- 轨道力学基本子程序，包括： 位置速度和轨道根数相互转换；地球引力场系数；JPL精密历表；RKF78数值积分器-Orbital mechanics subroutine, including: position, velocity and orbital elements are interchangeable Earth s gravitational field coefficient at JPL precise ephemerides RKF78 numerical integrat
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.
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.
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
EXERCISE_3_3
- 计算特定卫星轨道选择合适的力学模型，评估卫星上各种摄动力-Calculate specific satellite orbital mechanics to choose the right model, the assessment of a variety of satellite perturbation
Orbital-Mechanics-Project
- Mission Saturn to earth using gravity assist of jupiter-Mission Saturn to earth using gravity assist of jupiter
83043897Orbital-mechanics-basic-subroutine
- FORTRAN航天器轨道力学代码，是学习航天器轨道力学非常有用的资源(FORTRAN spacecraft orbital mechanics code)
[96.03.25][Project_Two Body Problem_C]
- two body problem orbital mechanics
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)
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