搜索资源列表
Reconfigurable-flight-control
- 精密控制结构需要满足先进飞机的使命和对其引航的要求。这就要求飞行器的性能必须满足在低空飞行，低速飞行和大迎角攻击性飞行，全天候，昼夜工作的条件，并且新的控制技术应该成熟。这项工作提出了飞行控制时，状态变量和控制输入是由预先确定的限制范围内的系统控制系统的设计理念。在设计过程使用动态规划的概念。其基本思想涉及非二次泛函最小化。由于一系列限制因素，建议使用光滑函数。同时提出了该综合方法的优点。我们利用对F-18战斗机的纵向控制配置来说明该设计方法。-Indirect adaptive control
jiyinzhouqi
- 基音是指发浊音时声带振动起的周期性, 而基音周期是指声带振动频率的倒数，通过AMDF计算音频的基音周期-Speech Pitch Period Estimation Based on AMDF
dwmusic
- 本程序为多维面阵的波达方位估计的程序，用于面阵俯仰角方位角定向-DOA DOA estimation procedures for multi-dimensional planar array of procedures for the azimuth orientation of the pitch angle of the plane array
noise-music
- 噪声子空间music方法。近场圆阵中俯仰角和方位角的联合估计，估计精度高，算法性能好。-Circular array of near-field pitch angle and azimuth joint estimation, estimation accuracy, the performance of the algorithm
CircleArrayBeamform
- 近场圆阵中俯仰角和方位角的联合估计，估计精度高，算法性能好-Circular array of near-field pitch angle and azimuth joint estimation, estimation accuracy, the performance of the algorithm
Pattern_plane3
- 近场圆阵中俯仰角和方位角的联合估计，估计精度高，算法性能好-Circular array of near-field pitch angle and azimuth joint estimation, estimation accuracy, the performance of the algorithm
12234445
- 采用卡尔曼滤波器对系统的俯仰角、 滚转角和航向角的误差进行最优估计；设计数据融合的判别准则，并根据判据的判断结果调整卡尔曼 滤波器中的量测信息，使系统可用于小型无人机的定高自主飞行-Kalman filter system pitch angle, roll angle and yaw angle error optimal estimation design data fusion criterion, and adjust according to the criterion of
Unitary--ESPRIT
- 新的2维角度估计的高分辨方法。该方法首先建立基于范数约束的最优化问题的目标函数；然后用迭代算法沿均匀面阵接收数据的方位向求最小化目标函数的稀疏解，得到方位、俯仰角耦合的空间角频率，并分离信号；最后对每个分离的信号，沿面阵俯仰向求稀疏解，得到信号的俯仰角，进而求得对应的方位角。-The new high-resolution 2-D angle estimation method. Firstly, the establishment of an objective function optimi
music
- 三维子空间music 方位角定义为与x轴的夹角，俯仰角定义为与z轴之间的夹角,俯仰角在0—90度，方位角0-180. 分辨不相关的两个角成功概率/估计偏差与SNR 最后进行谱峰搜索-Dimensional subspace music is defined as the angle and azimuth angle, pitch angle is defined as the x-axis and z-axis between the pitch angle of 0-9
zidongcejiyiinzhouqi
- 自动估测语音信号的基音频率。目前只能估计浊音，清音没有基音周期（会报错），基音周期取第二、三帧及以后的帧数。003和191分别是男声和女声的语音信号包。-Automatic estimation of the pitch frequency of the speech signal. Currently only estimated voiced, unvoiced no pitch (being given), take the second pitch, and after three fr
music_two
- 述是经典MUSIC算法的基本原理，许多限制是可以放宽或取消的。首先，关于均匀线阵的限制不是必须的，实际中可采用几乎是任意形状的阵列形式，只要满足在个独立信号源的条件下，矩阵具有个线性无关的列就可以了。其次，天线阵元在观测平面内无方向性这一点也不是必要的，而且还可以考虑三维空间的DOA估计问题，即不仅估计信号的方位角，还要估计它的俯仰角，当然MUSIC算法还用于频率、方位和俯仰的联合估计。-Above is the basic principle of the classical MUSIC al
fengyiu_v29
- 最大似然（ML）准则和最大后验概率（MAP）准则，利用贝叶斯原理估计混合logit模型的参数，包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- Maximum Likelihood (ML) criteria and maximum a posteriori (MAP) criterion, Bayesian parameter estimation principle mixed logit model, It comprises aircraft flight attitud
buifan_v46
- 欢迎大家下载学习，这是一个好用的频偏估计算法的matlab仿真程序,包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- Welcome to download the study, This is a useful frequency estimation algorithm matlab simulation program, It comprises aircraft flight attitude control, such as slip angle, tilt angle
fangqai_v79
- 欢迎大家下载学习，这是一个好用的频偏估计算法的matlab仿真程序,包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- Welcome to download the study, This is a useful frequency estimation algorithm matlab simulation program, It comprises aircraft flight attitude control, such as slip angle, tilt angle
qoulang
- 包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角，基于互功率谱的时延估计，isodata 迭代自组织的数据分析。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Based on the time delay estimation of power spectrum, Isodata iterative self-organ
pingpui_v49
- 现代信号处理中谱估计在matlab中的使用，Pisarenko谐波分解算法,包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- Modern signal processing used in the spectral estimation in matlab, Pisarenko harmonic decomposition algorithm, It comprises aircraft flight attitude control, such as slip angle,
kunkang
- ML法能够很好的估计信号的信噪比,FMCW调频连续波雷达的测距测角，包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- ML estimation method can be a good signal to noise ratio, FMCW frequency modulated continuous wave radar range and angular measurements, It comprises aircraft flight attitude control,
hingpan
- IMC-PID是利用内模控制原理来对PID参数进行计算，ML法能够很好的估计信号的信噪比,包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- The IMC- PID is using the internal model control principle for PID parameters is calculated, ML estimation method can be a good signal to noise ratio, It comprises aircraft
nangmui
- 使用起来非常方便，可以得到很精确的幅值、频率、相位估计，包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角。- Very convenient to use, You can get a very accurate amplitude, frequency, phase estimation, It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch
faigeng_v48
- 包含飞行器飞行中的姿态控制，如侧滑角，倾斜角，滚转角，俯仰角，现代信号处理中谱估计在matlab中的使用，数值分析的EULER法。- It comprises aircraft flight attitude control, such as slip angle, tilt angle, roll angle, pitch angle, Modern signal processing used in the spectral estimation in matlab, EULER numer