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Shell_Programming
SHELL概述;SHELL变量介绍;引用类型;控制流结构;函数;调试;(SHELL Overview SHELL variable is introduced reference type control flow structure function debugging )
- 2010-12-16 18:05:05下载
- 积分:1
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spi
关于spi的串行总线接口编程,实现同步传输(On the spi serial bus interface programming, synchronous transfer)
- 2010-01-01 14:42:42下载
- 积分:1
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hysdel-2.0.5-source.tar
说明: 由matlab开发的hybrid系统的描述语言,用于系统的建模、仿真、最优控制等。(from Matlab development of the hybrid system description language for the modeling, simulation, Optimal control.)
- 2006-05-10 03:53:47下载
- 积分:1
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DES
Data Encryption Standard
- 2017-10-10 07:04:32下载
- 积分:1
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DATABASEINFO
for capturing the image through webcam
- 2010-06-09 19:17:19下载
- 积分:1
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papr
LTE上行接入技术SC-FDMA的papr,其中包含采用不同调制方式和集中式、分布式接入技术的papr(LTE SC-FDMA uplink access technology of papr, which contains a different modulation mode and centralized, distributed access technology papr)
- 2010-12-27 21:05:38下载
- 积分:1
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omap_hwmod_33xx_data
Hardware modules present on the AM33XX chips.
- 2014-08-09 11:46:09下载
- 积分:1
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AAM
AAM is Active Aapearance Model that can be used for face tracking
- 2014-12-10 15:12:36下载
- 积分:1
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DstatcomDvr2
DVT + DSTATCOM MODEL USING SIMULINK
- 2015-01-06 20:12:21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