搜索资源列表
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
matlab_euler
- 航天器轨道计算中的eular方程应用函数。-Spacecraft orbit calculation eular equation application functions.
2012B
- 2012年全国研究生数学建模-基于卫星无源探测的空间飞行器的轨道估计，里面包括详细的设计求解过程，含有matlab解算的M文件。-2012 National Mathematical Modeling graduate- satellite-based passive probe spacecraft orbit estimate, which includes detailed design solution process, the file containing the M matlab
Modeling-of-trajectory
- Matlab进行再入式飞行器轨道建模与仿真，建立各种模型，最后获得飞行器的动力学模型，并调用龙格库塔函数求解该微分方程初值问题。-Matlab for reentry spacecraft orbit modeling and simulation, the establishment of various models, and finally obtain the dynamic model of the aircraft, and call the Runge-Kutta function
guidaozhuanhuan
- 航天器动力学中用于计算轨道转换的MATLAB程序，包括平面的转换为空间的与空间的转换为平面轨道。-Spacecraft Dynamics used to calculate the orbit convert MATLAB program, including the conversion plane converted to space and space for flat track.
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
dinggui
- 使用MATLAB，根据轨道根数实现航天器定轨条件-Using MATLAB, based on the number of spacecraft to achieve orbit Orbit conditions
untitled3
- 航天器轨道动力学MATLAB仿真，霍曼转移，Simulink- Spacecraft orbit dynamics MATLAB simulation, Hohmann transfer
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
1
- 关于航天器航天器轨道力学轨道参数计算，利用开普勒定律计算六个轨道根数等(The orbit parameters of spacecraft, ft and spacecraft are calculated)