# im trying to model the drive train model of wind turbine, i need to get oscillation and the steady state waveform

조회 수: 6(최근 30일)
peddada sandhya rani 2023년 3월 25일
답변: Sam Chak 2023년 3월 25일
dwt/dt=1/2Ht(Tt-Tsh)
dwr/dt=1/2Hg(Tsh-Te)
Tsh=k*thetatw+c*dtheta_tw/dt
dtheta_tw/dt=welb(wt-wr)
thetatw=3.35
wt=1
wr=1

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### 채택된 답변

VBBV 2023년 3월 25일
Provide all inputs to the equations used for modeling the drive train,
clc
clear all
close all
a=3.2; %input('Enter the a = ');
b=1.5; %input('Enter the b = ');
c=.1;%input('Enter the c = ');
%initial condition
theta_0=[a,b,c];
t_span=linspace(0,100,100);
[t,results]=ode45(@(t,theta)ode_fun(t,theta),t_span,theta_0);
subplot(211)
plot(t,results(:,2));
subplot(212)
plot(t,results(:,3));
xlabel('t')
ylabel('wt&wg')
function [dtheta_dt]= ode_fun(t,theta)
Tt=1;
Te=0.78;
f=50;
welb=2*pi*f;
Ksh=0.3;
Csh=0.01;
Ht=4;
Hg=0.1*Ht;
wt=theta(1);
wg=theta(2);
thetatw=theta(3);
dthetatw_dt=welb*(wt-wg);
thetatw=3.35;
wt=0.1;
wr=0.01;
c = 0.1; % give damping constant factor
k = 2.6e8; % give flexural stiffness of gear train , e.g. shown
dtheta_tw_dt=welb*(wt-wr);
Tsh=k*thetatw+c*dtheta_tw_dt;
dwt_dt=(1/2)*Ht*(Tt-Tsh); % what are these for ? another model ?
dwr_dt=(1/2)*Hg*(Tsh-Te); % this one too
Dwt_dt=((Tt/(2*Ht))-((Ksh/(2*Ht))*thetatw)+((Csh/(2*Ht))*(welb*(wt-wg)))); % check these equations
Dwg_dt=(((Ksh/(2*Hg))*thetatw)-((Csh/(2*Hg))*(welb*(wt-wg)))+(Te/(2*Hg))); % check these
dtheta_dt=[dthetatw_dt;Dwt_dt;Dwg_dt];
end

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### 추가 답변(1개)

Sam Chak 2023년 3월 25일
In the absence of the effects of the constants and in the original math model, then the system is stable.
If oscillations are desired, then you need to inject some manipulated variables so that the system behavior can be changed. I'm unfamiliar with your system. In physical systems, the manipulated variables can forces, torques, voltage sources, etc.
theta_0 = [0.1, -0.2, 1];
t_span = linspace(0, 10, 10001);
options = odeset('AbsTol', 1e-16, 'RelTol', 1e-12);
[t, theta] = ode45(@(t,theta) ode_fun(t, theta), t_span, theta_0, options);
subplot(311)
plot(t, theta(:,1)), grid on, ylabel('\omega_{t}')
subplot(312)
plot(t, theta(:,2)), grid on, ylabel('\omega_{g}')
subplot(313)
plot(t, theta(:,3)), grid on, ylabel('\theta_{tw}'), xlabel('t')
function [dtheta_dt]= ode_fun(t, theta)
% Parameters
Tt = 1;
Te = 0.78;
f = 50;
welb = 2*pi*f;
Ksh = 0.3;
Csh = 0.01;
Ht = 4;
Hg = 0.1*Ht;
wt = theta(1);
wg = theta(2);
thetatw = theta(3);
% Test 1: without manipulated variables, without constant disturbances
% dwt_dt = 0*Tt/(2*Ht) - Ksh/(2*Ht)*thetatw - Csh/(2*Ht)*welb*(wt - wg);
% dwg_dt = Ksh/(2*Hg)*thetatw + Csh/(2*Hg)*welb*(wt - wg) - 0*Te/(2*Hg);
% dthetatw_dt = welb*(wt - wg);
% Test 2: with manipulated variables
A = [ -pi/8 pi/8 -3/80;
5*pi/4 -5*pi/4 3/8;
100*pi -100*pi 0];
B = eye(3);
p = [-1, -2i, +2i]; % desired eigenvalues
K = place(A, B, p);
% Manipulated variables
u1 = - K(1,:)*theta - Tt/(2*Ht); % also cancel out effect of Tt/(2*Ht)
u2 = - K(2,:)*theta + Te/(2*Hg); % also cancel out effect of Te/(2*Hg)
u3 = - K(3,:)*theta;
dwt_dt = Tt/(2*Ht) - Ksh/(2*Ht)*thetatw - Csh/(2*Ht)*welb*(wt - wg) + u1;
dwg_dt = Ksh/(2*Hg)*thetatw + Csh/(2*Hg)*welb*(wt - wg) - Te/(2*Hg) + u2;
dthetatw_dt = welb*(wt - wg) + u3;
% Reorder the sequence because thetatw = theta(3)
dtheta_dt = [dwt_dt;
dwg_dt;
dthetatw_dt];
end

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