Search - pressure control matlab

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[Other resource] Test_ABS DL : 0: 这是我利用Matlab编写的汽车ABS测试软件他可以通过输入压力、车速以及轮速计算出合理的控制量-Matlab prepared by the ABS software testing can be done by the importation of pressure, speed and the wheel speed calculation of a reasonable amount of control
Update : 2008-10-13 Size : 1.8kb Publisher : 王伟
[transportation applications] Test_ABS DL : 0: 这是我利用Matlab编写的汽车ABS测试软件他可以通过输入压力、车速以及轮速计算出合理的控制量-Matlab prepared by the ABS software testing can be done by the importation of pressure, speed and the wheel speed calculation of a reasonable amount of control
Update : 2025-02-19 Size : 2kb Publisher : 王伟
[matlab] FluidPipelineSimulinkModels DL : 0: These Simulink blocks contain transfer functions that model the pressure and flow transients for axisymmetric 2D viscous flow of a compressible fluid in a straight rigid circular cross section pipelines. Three models are available: (1) pressures at the ends (2) flow rates at the ends (3) pressure at one end and flow rate at the other Filtering is incorporated to reduce numerical oscillation (Gibbs phenomenon). See J. Dyn. Systems, Meas. & Control vol 122 (2000) pp. 153-162.
Update : 2025-02-19 Size : 5kb Publisher : leiming691128
[matlab] PID DL : 0: 螺旋桨PID控制 In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate. -PID control of the propeller In response to constant pressure to design more efficient, faster, smaller, and better systems, engineers are constantly looking for ways to improve existing designs or replace them with better ones. Facing large fuel costs, the aerospace industry in particular has been researching alternative designs to increase fuel efficiency and performance. One such alternative is the development of reconfigurable aircraft wings. These wings would be able to adapt to the current environment increasing lift or reducing drag when appropriate.
Update : 2025-02-19 Size : 1kb Publisher : 王晨至
[Graph Drawing] B-spline-surface DL : 0: 这是在MATLAB-2008a环境下编写的B样条曲面生成程序，可以通过调整节点矢量和控制顶点来调整曲面形状。-This is a MATLAB-2008a environment, prepared by B-spline surface generation program, you can adjust the knot vector and control points to adjust the surface shape.
Update : 2025-02-19 Size : 492kb Publisher : 小胡
[Algorithm] Fuel_Supply_System DL : 0: 油料传送系统的MATLAB的三维仿真程序。针对皮带运动各种情况分析。-This file contains a model of a simple fuel system modeled using Simscape and SimHydraulics. Pumps and valves control the flow between fuel tanks. The pressure drop along the fuel lines is dependent upon the elevation at the ends of the line. The model includes a set of test scenarios that include varying environmental conditions and failure events for components in the system. A MATLAB script automates the execution of these tests, and produces a plot to show how the system performed in each test.
Update : 2025-02-19 Size : 48kb Publisher : 林真天
[Compress-Decompress algrithms] Flutter DL : 2: 这个程序演示了如何应用耦合结构空气动力问题，通过Matlab编程，分析了飞行器机翼颤振等问题。-This model demonstrates how to implement a coupled structural-aerodynamic problem. The wing, otherwise rigid, is allowed to pitch and plunge. The motion of the wing is defined using SimMechanics blocks. The aerodynamic model is a simple, quasi-steady formulation. Dynamic pressure is manipulated by varying the Mach number & Altitude. You can also vary the CG location of the wing by double clicking on the picture of the BACT subsystem. The structural, mass, and aerodynamic properties all come from the following "Modeling the Benchmark Active Control Technology Wind Tunnel Model for Application to Flutter Suppression" by Martin R. Waszak of NASA Langley. Automatic flutter detection is implemented via a state-machine in Stateflow.
Update : 2025-02-19 Size : 78kb Publisher : 王振坤
[matlab] Standard-atmospheric-program-code DL : 0: 用matlab/m文件编写的计算标准大气压小程序，非常实用，可以用于各种飞行器控制设计等方面的仿真，m文件编写很容易转换成c/c++，有问题请留言。-Written using matlab/m file calculation standard atmospheric pressure of small procedures, very useful, can be used for simulation of various aircraft control design, m document can be easily converted into c/c++, have any questions please leave a message
Update : 2025-02-19 Size : 1kb Publisher : 周胜俞
[matlab] PID3 DL : 0: 各种经典PID的MATLAB程序，主要涉及温度控制，压力控制，液位控制等-All kinds of classic PID MATLAB procedures, mainly related to the temperature control, pressure control, level control, etc
Update : 2025-02-19 Size : 552kb Publisher : 赵丹
[matlab] program 3 DL : 0: Formalization and research of model of linear optimization of the state of difficult object on the example of subsystem of cardiovascular disease risk. Criterion of optimization: the risk class(An optimization criterion was formed for the risk of cardiovascular disease, where the control of the system was applied using variables representing systolic blood pressure and maximum heart rate during the stress test. The reaction of the optimal result to the variation of the accidental influence restrictions was investigated. It was developed an application for more convenient work with the model.)
Update : 2025-02-19 Size : 30kb Publisher : Dimon060195
[matlab] ZVS_full_bridge DL : 0: 基于MATLAB/SIMULINK的零电压移相全桥DC/DC变换器仿真。恒压控制。PI。已经过修改调试，效果良好。可直接用于借鉴学习。模型基于matlab R2016b.(Simulation of zero voltage phase shifted full bridge DC/DC converter based on MATLAB/SIMULINK. Constant pressure control. PI. It has been modified and debugged, and the result is good. Can be directly used for reference learning. The model is based on MATLAB R2016b.)
Update : 2025-02-19 Size : 27kb Publisher : a1028650284