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LQR-for-vehicule-active-suspension
LQR for active suspension system _ Matlab code
- 2011-11-10 12:04:25下载
- 积分:1
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image-encoding
冈萨雷斯数字信号处理书中部分matlab源码,和示例(image encoding)
- 2015-04-15 10:46:05下载
- 积分:1
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DEA例子
说明: matlab对DEA编程Programming DEA with MATLABmatlab对DEA编程(Programming DEA with MATLAB)
- 2019-03-27 14:16:34下载
- 积分:1
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Modified_SPWM
simulink model of an innovative sinusoidal pulse width modulation technique. try to verify the performance. it is for study purpose..
- 2011-09-22 23:20:59下载
- 积分:1
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matlab
denoise and wacelet analysis of signals
- 2012-11-09 15:46:42下载
- 积分:1
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exm09321_1
对matlab初学者很有帮助,尤其是simulink的爱好者。(helpful to beginners Matlab, Simulink is particularly fond.)
- 2007-05-08 16:12:59下载
- 积分:1
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VISUM-Exercise-for-Monday
Visum Exercise for Monday no use of matlab
- 2011-10-05 06:19:47下载
- 积分:1
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optical_tools_matlab2
matlab中的光学工具,实现光学仿真实例源代码(第二部分)(matlab opyical tool)
- 2013-08-23 19:52:15下载
- 积分:1
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emd
matlab经验模态分解 emd 工具包 包含emd常用函数,可用于机械设备故障诊断(Matlab empirical mode decomposition toolkit can be directly used in mechanical equipment fault diagnosis)
- 2019-06-20 21:46:43下载
- 积分:1
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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 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)
- 2021-01-28 10:38:35下载
- 积分:1