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KARIMQPSK
This code simulates QPSK modulation on base band. This code has been written on Matlab and it will be very useful I think! :)
- 2013-12-05 06:59:52下载
- 积分:1
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flight-engineer
飞行器在某高度平飞时舵面偏角和飞行马赫数之间的关系(it describes the relationship between elevator declination and flight mach number,when flight fly on some hight.)
- 2013-12-10 23:37:28下载
- 积分:1
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QPSK
说明: QPSK(四进制相移键控)信号的产生及调制解调过程(经高斯和瑞利信道)的仿真(QPSK (quaternary phase shift keying) signal generation and modulation and demodulation process (by the Gaussian and Rayleigh channel) Simulation)
- 2011-02-24 10:34:45下载
- 积分:1
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Multiset
A collection that supports order-independent equality, like Set, but may have duplicate elements.
- 2014-05-21 11:19:04下载
- 积分:1
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fuzzy-identification-
fuzzy identification
- 2014-10-18 18:22:21下载
- 积分:1
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QOSTBC
基于天线选择的准正交空时分组码的自适应分析。(Analysis of adaptive antenna selection quasi-orthogonal space-time block codes.)
- 2015-03-23 20:16:10下载
- 积分:1
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bpskofdm_rect
BER simulation of BPSK OFDM with a rectangular filter
- 2010-06-24 17:21:36下载
- 积分:1
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flappybird
说明: a game
- 2015-04-21 16:41:05下载
- 积分:1
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非线性动力学 nonlinear
非线性动力学、分岔 Matlab 程序实现,弹簧质量系统在简谐激励作用下的受迫振动,弹簧的恢复力F与变形x的关系为F=kx3,动力学方程为...30cosmxcxkxFwt++= 其中,给定参数,1m=,0.3c=,1.0k=,1w=,初始条件为(0)3.0x=,.(0)4.0x=设系统的动态参数为F0,绘出系统状态变量随参数变化分岔图,绘图参数对应的系统各周期及混沌状态的时间历程图、相轨迹图、Poincare映射图(Nonlinear dynamics, bifurcation Matlab program, the forced vibration spring-mass system under harmonic excitation, spring restoring force F and deformation x relationship the F = kx3, kinetic equation for ... 30cosmxcxkxFwt++ = wherein the given parameters, 1m = 0.3C = 1.0k = 1W =, initial condition (0) 3.0x = (0) 4.0x = set of the dynamic parameters of the system for the F0, plotted system status system cycle and chaotic state variables with parameter changes bifurcation diagram, drawing parameters corresponding time course of the phase trajectories, Poincare map)
- 2021-03-06 19:29:30下载
- 积分:1
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exp4
说明: 把激光陀螺捷联惯导系统和GNSS接收机固联于实验车实验仓中,接收机天线固联在实验车实验仓上方,车载计算机实时接收和采集惯导系统、卫星导航接收机的原始数据,在郊外开阔公路进行车载实验。
通过matlab编程实现卫星导航伪距单点定位、INS/GPS松组合导航的全过程。
1)卫星导航单点定位测速:利用采集得到的接收机时间、伪距、多普勒频移数据,要求进行单点定位、测速解算,输出接收机的位置、速度随时间的变化曲线,并给出位置、速度误差曲线;
2)松组合导航:结合惯导解算和卫星接收机单点定位测速,要求采用Kalman滤波器实现惯导/卫星位置、速度组合导航解算,滤波器维数至少包括惯导的位置、速度、姿态角9维。将组合导航后的姿态角与纯惯导的姿态角进行对比分析,给出位置、速度误差曲线。(The laser gyro strapdown inertial navigation system and GNSS receiver are fixed in the experimental compartment of the experimental vehicle. The antenna of the receiver is fixed above the experimental compartment of the experimental vehicle. The on-board computer receives and collects the original data of the inertial navigation system and satellite navigation receiver in real time, and carries out on-board experiments on the suburban open highway.)
- 2021-03-25 17:19:14下载
- 积分:1