-
tcm_psk
用MATLAB程序实现了tcm_8psk的中频调制解调,有性能检测以及加入了非线性因素,很详细,毕设用的程序,比较实用。(Using MATLAB program implements tcm_8psk IF modulation and demodulation, a performance test and joined the non-linear factors, very detailed, complete set with the procedure more practical.)
- 2010-07-01 10:18:57下载
- 积分:1
-
OFDM_10G_transmiter
matlab 代码实现的OFDM发射机,matlab 代码实现的OFDM发射机(OFDM orthogonal frequency division multiplexing)
- 2011-05-24 20:35:24下载
- 积分:1
-
BCC
this program is a code for DEA, BCC model in matlab programming . I hope that can help you.
- 2013-09-23 21:32:44下载
- 积分:1
-
LMS2
数字信号处理的自适应算法,最陡下降法与LMS法比较,画出两者收敛曲线(Adaptive digital signal processing algorithms, steepest descent method with the LMS method, draw the two curves converge)
- 2007-10-23 12:18:39下载
- 积分:1
-
flops
matlab matrix processing functions
- 2010-12-08 01:50:41下载
- 积分:1
-
201400525-201400564-P1
Binary to decimal floating point conversion
- 2015-03-25 18:06:23下载
- 积分:1
-
The-detection-of-high-speed-targets
说明: 怎么来进行高速运动雷达弱小目标检测方法研究呢(How to carry out high-speed movement of Small Target Detection Radar it)
- 2011-03-09 11:26:54下载
- 积分:1
-
FDTD
用matlab实现的时域有限差分法程序,模拟了金属槽的电势分布。(Matlab implementation of the finite difference time domain method program to simulate the potential distribution of the metal tank.)
- 2012-05-14 20:53:02下载
- 积分:1
-
适用于捷联惯导系统(SINS)初始对准的新算法self-alignment
在运载体运动情况下,提出了一种适用于捷联惯导系统(SINS)初始对准的新算法,该算法以惯性空
间为过渡参考基准,即建立了初始时刻惯性坐标系(i0系)和初始时刻捷联惯组惯性坐标系(ib0系)两个惯性坐标
系。将捷联惯组坐标系(b系)与导航坐标系(n系)之间的初始对准姿态矩阵的实现分解为三步骤:(1)通过地理
位置和初始对准时间求解i0系至n系的变换矩阵 (2)通过惯导比力方程变形,引入测速仪速度辅助,求解从ib0
系至i0系的常值变换矩阵 (3)使用姿态更新算法实时计算b相对于ib0系的变换矩阵。最后,载车运动环境下的
初始对准试验结果表明航向角对准精度达到了0.1b(1R)。
(On the moving base, a new initial alignment algorithm for strapdown inertial navigation system
(SINS) is proposed. In this algorithm, two special inertial frames, the initia-l time inertial frame (i0frame) and
the initia-l time SINS body inertial frame (ib0frame), are defined and are selected as transition reference frames.
The calculation of initial alignment direction cosine matrix (DCM) between SINS body frame (bframe) and nav-
igation reference frame (nframe) is expanded into three parts: (1) the DCM betweeni0frame andnframe is
easily obtained via local geographical coordinates and initial alignment time (2) by expressing SINS specific
force equation inbframe and by the aid of external velocity log, the constant DCM fromib0frame toi0frame is
achieved (3) attitude updating using gyro samples gets the DCM betweenbframe andib0frame. In the end,
some vehicular tests are carried out on the moving base and the accuracy of azimuth reaches about 0.1b(1R).
)
- 2015-08-23 07:58:59下载
- 积分:1
-
Multi-bus-based-simulation-of-aircraft-electrical-
基于多总线的飞机电气故障模拟实验系统设计Multi-bus-based simulation of aircraft electrical system failure(Multi-bus-based simulation of aircraft electrical system failure)
- 2011-01-10 19:12:22下载
- 积分:1