搜索资源列表
Matlabtoolbox_space
- Matlab航天器工具箱，用于轨道计算，2D或3D的平面显示，包含计算多卫星轨道动力学模型和地面覆盖分析等-Matlab toolbox spacecraft for orbit calculation, 2D or 3D graphic display, including the calculation of multi-satellite orbital dynamics analysis model and floor coverings
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!
drawing
- 使用matlab绘制原子轨道图和电子云图-Drawing atomic orbital and electronic cloud using MATLAB
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
Orbit
- 卫星轨道机动模拟仿真matlab程序，应用GPS数据进行具体分析。-Matlab simulation of satellite orbit maneuver, application specific analysis of GPS data.
xyz_elements
- matlab程序，实现卫星的两行轨道要素和位置速度矢量的互转，用于轨道动力学计算-matlab program to realize the satellite orbital elements and position of two lines of the velocity vector of the system conversion, calculated for the orbital dynamics
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.
matlab
- 轨道根数与状态向量的转换，已知状态向量求解轨道根数！-Orbital and state vector conversionSolving the state vector is known orbital elements ! 。
orbitalcalc
- Orbital calculation for satellite communication GUI in MATLAB
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
aircraft-three-orbital-degrees
- 通过matlab仿真建立某飞行器三自由度轨道-By establishing an aircraft three matlab simulation orbital degrees of freedom
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
OrbitalElements
- Matlab code for calculating orbital elements
cowell
- orbital motion of Earth satellites using Cowell's method and equations of motion in rectangular coordinates
Applied-Orbital-master
- Homeworks for aerospace dynamics courses with matlab solutions
cb206
- Various kalman filter design, Including orbital maneuvering simulation, initial orbit calculation, matlab prepared cellular automata.
ken-V7.7
- Partially achieved tracking speed iterative relaxation algorithm, A window function design FIR digital band-pass filter, Including orbital maneuvering simulation, initial orbit calculation.
vj421
- Use matlab intelligent predictive control algorithm, Including orbital maneuvering simulation, initial orbit calculation, The true extent of the value of the intermediary measure, measure the true extent of the agency based on the value of image segm
orbit
- 编程仿真连续小推力实现GTO到GEO的三阶段转移过程，其中推力器的推力大小为0.8N，轨道机动的起始点为GTO的远地点。GTO轨道的升交点赤经为0度，近地点角距为90度。 GTO轨道： ph:185km，ah：35786km，i：28.5°，GEO轨道：h：35786km，i：0°。 卫星质量为6600kg，从GTO到GEO，采用5000s的推力器。取地球半径为6378km，g取值为9.8m/s^2(The three stage transfer process from GTO to G