搜索资源列表
sldemo_f14
- This demonstration models a flight control for the longitudinal motion of a Grumman Aerospace F-14 Tomcat. First order linear approximations of the aircraft and actuator behavior are connected to an analog flight control design that uses the pilot
bpannpid
- 一个神经网络PID控制例子 2C控制对象为一个直升机俯仰轴的角度控制 2C数学模型为二阶传递函数-PID control of a neural network control 2C an example of a helicopter for the angle of pitch-axis control 2C mathematical model for the second-order transfer function
pitch_control
- Pitch Control for Wind generator
DFIG
- another pitch control for wind generators
Wind_Turbine_Model
- 详细的双馈发电机模型，包括变桨系统、偏航系统、控制系统、齿轮箱等。-Detailed model of doubly-fed generator, including the pitch system, yaw system, control system, gear boxes.
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
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
Semi-Supervised-Kernel-Based-Fuzzy
- 研究半监督学习的模糊核聚类方法用于变速箱早期故障诊断的方法。故障特征不明显、样本差异小是机械故障早期检测的 难点， 基于半监督学习的核聚类方法利用少量已知模式的样本， 结合大量未知模式的样本进行半监督学习， 得到较好的识别效果。-In this paper, motion control method of semi-closed CNC method is presented for gear-box fault early detection. The difficulty mach
daima
- 课设作业，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-Attitude control of spacecraft Contains the pitch angle, roll angle，Tilt angle, sideslip angle
missile-3-channel-simulink
- 本文主要通过极点配置法，设计了导弹三通道的控制系统，整体性能达到了设计的基本要求，在导弹垂直上升阶段及俯仰阶段，分别选取特征点进行仿真，达到了垂直发射中姿态角控制的要求。但是，采用极点配置法设计的控制律仍存在许多不足，短时间内具有良好的性能，而某一时刻之后系统将面临着严重的振荡。可以考虑采用其它方法重新设计，或是多种控制方法的结合，扬长避短，可获得更为理想的效果。-In this paper, the pole placement method, the design of a missile
matlab
- 飞机俯仰电传操纵系统设计，matlab仿真-Aircraft pitch fly-by-wire control system design, matlab simulation
variable-pitch-control-system
- 这是关于风力发电机变桨距系统的一篇文章，希望对大家有所帮助。-This is about the variable pitch wind turbine system in an article, we want to help.
PitchSystem180to90
- pITCH CONTROL SYSTEM OF TURBINE WITH CLOSED LOOP SPEED POSITION AND CURRENT CONTROL LOOP
RBF_PID
- 该程序是基于RBF神经网络调节PID三个参数，实现风力机变桨距控制效果。其中包含风力机的仿真模型，控制效果较好。-The program is based on the RBF neural network regulator PID three parameters, and wind turbine pitch control. Which includes wind turbine simulation model, control is better.
WIND-DFIG-PITCH-ANGLE-q-CONTROL
- DFIG wind system with pitch angle controland reactive power control
语音分析
- 实现语音分析的功能，基音提取，波形、能量、过零、基音周期对照图及说明(To achieve the function of speech analysis, pitch extraction, waveform, energy, zero crossing, pitch, control chart and instructions)
Pitch_Control_Ideal_Testrig
- Simulink for pitch control for turbine system (ideal testing).
pitch_control
- pitch control of double fed induction generator
variable-pitch-control-system
- variable pitch mppt control
PMSGWind
- 以直驱式永磁同步风力发电机为研究对象，在Matlab/simulink平台建立了风力机模型、传动系统模型，采用变桨距控制。(Taking the direct drive permanent magnet synchronous wind turbine as the research object, the wind turbine model and the transmission system model are established on the MATLAB / Simulink