-
dtsspMatlabAll
This is transfer function for matlab.
- 2009-03-19 05:06:37下载
- 积分:1
-
h_load_callback
Good file to test for nothing.
- 2011-07-21 22:30:56下载
- 积分:1
-
diktat-gabungan-matlab
matlab tutorial berbahasa indonesia
- 2013-09-07 05:34:24下载
- 积分:1
-
yaogan
基于形态学方法的图像分割文件,.m的源代码(Based on morphological image segmentation file,. M of the source code)
- 2011-09-29 20:53:26下载
- 积分:1
-
MeanShiftCluster
mean shift clustering
- 2014-10-23 19:06:44下载
- 积分:1
-
BSS
一种基于稀疏变量的欠定盲分离算法,很好用,大家试一下。(Underdetermined blind separation algorithm based on sparse variables)
- 2014-12-23 14:57:07下载
- 积分:1
-
GPS-Matlab
一个GPS课程的全部代码,含有数据!很实用(MATLAB GPS SCRIPTS-- Charles Meertens and Doug Miller, U. Utah 3Jan95
These scripts were developed for/during a class in GPS and Active Tectonics
Department of Geology and Geophysics, U. Utah, Spring, 1994
EXAMPLE RINEX Files (the only ones guaranteed to work this release)
CUR10911.94N
CUR10911.94O
PAR10910.94N
PAR10910.94O
Main Program scripts:
gpshora.m -- function to calculate Modified Julian Day, Homework#1
HW2.m -- Homework#2 read RINEX observation file and plot C/A code vrs. time
HW3_plt.m-- Homework#3 read RINEX navigation file, plot satellite positions
HW3_3dplt.m-- Same as HW3_plt.m, but 3d position plots
HW4.m-- Homework#4 calculate and plot station position as function of time
Functions called:
calc_nav.m-- calculate satellite position
calc_pos1.m-- calculate station position
constants.m-- GPS constants
coords.m-- convert x,y,z coordinates to lat, long, height
date2j.m-- calculate MDJ
eccenr.m-- calculate "E" anomally
read_nav.m-- Read RINEX Nav file
r)
- 2020-06-30 23:40:02下载
- 积分:1
-
sifu3dot10
液压控制系统仿真,应用于液压伺服系统,位置伺服系统!(The hydraulic control system simulation used in hydraulic servo system, the position servo system!)
- 2012-10-07 22:05:58下载
- 积分:1
-
exm1
BPSK的Matlab简单仿真,得到理想情况下的误码曲线(BPSK仿真之matlab)
- 2010-05-31 16:50:15下载
- 积分:1
-
F16_dyn
F16开环动力学系统模型。输入为油门及三个舵面控制,以及系统低阶、高阶选择器。输出为飞机飞行状态以及油门大小。采用Quaternion四元素法,可以有效避免俯仰角theta达到90°时数学奇异现象。(F16 open-loop dynamic system model. Throttle input and three rudder control, and system low, high selector. Output is the size of aircraft status, and throttle. Quaternion method using the four elements, can effectively avoid the pitch angle theta to 90 °, mathematics strange phenomenon.)
- 2011-09-30 11:04:51下载
- 积分:1