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Description: GEO表达谱的相关matlab源程序及数据文件举例
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Size: 1888261 |
Author: rain |
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Description: 建立GEO和LEO的轨道，并计算他们间方位角和俯仰角速度及加速度，多普勒频移等重要参数。-established GEO and LEO orbits, and calculate their azimuth and pitch between angular velocity and acceleration, Doppler frequency shift and other important parameters.
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Size: 28672 |
Author: 韩成 |
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Description: GEO表达谱的相关matlab源程序及数据文件举例-GEO expression profiling relevant matlab source code and data files, for example
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Size: 1888256 |
Author: rain |
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Description: 图像融合算法，是由教科书推荐下载的学习资料。尤其适用于地球信息处理领域的研究人员。-Image fusion algorithm, is recommended by the textbook learning materials downloaded. Applies in particular to the field of geo-information processing researchers.
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Size: 50176 |
Author: zeng |
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Description: Matlab code earth coordinates transformation-Matlab code Earth fix coordinates to geodetic coordinate transform
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Size: 1024 |
Author: David |
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Description: geo软件接收机的功能实现 matlab代码-geo functions matlab
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Size: 13312 |
Author: adams_bing |
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Description: matlab地理图形处理。中国地图，非常重要-matlab geography graphics processing
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Size: 97280 |
Author: 林晨 |
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Description: 用matlab进行有限元编程资料，需要用gmsh对geo文件进行网格划分，可更改各项参数后评价区域的传热性能-Finite element program data using matlab, need for geo file gmsh meshing, parameters can be changed after the heat transfer performance uation area
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Size: 1574912 |
Author: Gao |
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Description: 使用MATLAB编写了回归轨道卫星、GEO卫星、地球静止轨道卫星星下点轨迹运动仿真模拟程序-the simulazation of the footprient of the satlite SAR
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Size: 2048 |
Author: 李德伟 |
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Description: 使用遗传算法，对于GEO卫星监控平台，求解卫星的最优轨道(Using the genetic algorithm, the GEO satellite monitoring platform is used to solve the optimal orbit of the satellite)
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Size: 2048 |
Author: vincent123
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Description: gprmax的out文件和geo文件的输出模型，可以直接在matlab中带入(The gprmax out file and the output model of the geo file can be directly brought into the MATLAB)
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Size: 7168 |
Author: jack落落 |
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Description: 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 GEO is realized by simulation and continuous small thrust. The thrust of the thruster is 0.8N, and the starting point of orbital maneuver is the apogee of GTO. GTO orbit RAAN is 0 degrees, 90 degrees for the argument of perigee.
GTO orbit: ph:185km, ah:35786km, i:28.5, GEO orbit: h:35786km, i:0.
The mass of the satellite is 6600kg, from GTO to GEO, using the 5000S thruster. The radius of the earth is 6378km, and the value of G is 9.8m/s^2)
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Size: 45056 |
Author: 大柚子 |
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Description: 基于matlab的地质楔型体剖面正演记录，适合地球物理学（勘查技术与工程）学生参考使用(Geo wedge profile forward recording based on MATLAB is suitable for students in Geophysics (exploration technology and Engineering).)
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Size: 1058816 |
Author: upcsen |
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