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发表于 2007-8-20 20:38
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子程序:
function dq=Rotors_System_Sub_Func(t,q) %???
global BN Nb1 Nb2 w1 w2 Ro1 Ri1 Ro2 Ri2 %????
r01=0.00002;%m ?????
%r02=0.00005;%m
m1=7.86;%kg ??
m2=11.93;%kg
W1=m1*9.8;%N ??
W2=m2*9.8;%N
Kb1=4.6346e10;%N/m^1.5 %??
Kb2=3.4953e9;%N/m^1.1
F=1485;
F1 = 1485/2;
delta_i=1.2443*w2^2*1e-11;
delta_e=2.2183*w1^2*1e-11;
Dm=(117+133.3)/2;
wc=(w2*(1-8/Dm)+(1+8/Dm)*w1)/2;
delta_o=4.912*wc^2*1e-14;
delta_F=8.10*F1^0.925/7.8^0.85*1e-8;
r02=0.00005-(delta_i-delta_o-delta_e-delta_F);
%q %???????Q??
Fx11=0;
Fy11=0; %??????
Fx22=0;
Fy22=0;
for i=1:Nb1
sita(i)=2*pi/Nb1*(i-1)+BN/Nb1*w1*2*pi*t; %??
Deformation(i,1)=q(1,1)*cos(sita(i))+q(2,1)*sin(sita(i))-r01; %??
if Deformation(i)<=0
Deformation(i)=0; %?????????
end
fx11=Kb1*(Deformation(i))^1.5*cos(sita(i));
fy11=Kb1*(Deformation(i))^1.5*sin(sita(i)); %?
Fx11=Fx11+fx11; %??
Fy11=Fy11+fy11;
%sita2(i)=2*pi/Nb1*(i-1)+BN/Nb1*w2*2*pi*t;
%Deformation2(i,1)=q(3,1)*cos(sita2(i))+q(4,1)*sin(sita2(i))-r01;
%if Deformation2(i)<=0
% Deformation2(i)=0;
%end
%fx22=Kb1*(Deformation2(i))^1.5*cos(sita2(i));
% fy22=Kb1*(Deformation2(i))^1.5*sin(sita2(i));
% Fx22=Fx22+fx22;
% Fy22=Fy22+fy22;
end
Fx12=Fx11;
Fy12=Fy11;
%Deformation %????? ????
%???????
Fx21=0;
Fy21=0;
for j=1:Nb2
sita(j)=2*pi/Nb2*(j-1)+(Ro2/(Ro2+Ri2)*w1+Ri2/(Ro2+Ri2)*w2)*2*pi*t;
Deformation1(j,1)=q(3)*cos(sita(j))+q(4)*sin(sita(j))-r02;
if Deformation1(j)<=0
Deformation1(j)=0;
end
fx21=Kb2*(Deformation1(j))^1.1*cos(sita(j));
fy21=Kb2*(Deformation1(j))^1.1*sin(sita(j));
Fx21=Fx21+fx21;
Fy21=Fy21+fy21;
end
%Fx22=0;
%Fy22=0;
for k=1:Nb1
sita(k)=2*pi/Nb1*(k-1)+BN/Nb1*w2*2*pi*t;
Deformation2(k,1)=q(3,1)*cos(sita(k))+q(4,1)*sin(sita(k))-r01;
if Deformation2(k)<=0
Deformation2(k)=0;
end
fx22=Kb1*(Deformation2(k))^1.5*cos(sita(k));
fy22=Kb1*(Deformation2(k))^1.5*sin(sita(k));
Fx22=Fx22+fx22;
Fy22=Fy22+fy22;
end
P=1470;
Cx11=1500;Cy11=1500; %???
Cx12=2500;Cy12=2500;
Cx21=2000;Cy21=2000;
Cx22=7000;Cy22=7000;
%dq(1:4,1)=q(5:8,1);
dq(5:8,1)=[-1/m1*((Cx11+Cx12)*q(5,1)+Fx11+Fx12-(W1+Fx21+Cx21*q(7,1)));...
-1/m1*((Cy11+Cy12)*q(6,1)+Fy11+Fy12-(Fy21+Cy21*q(8,1)));...
-1/m2*((Cx21+Cx22)*q(7,1)+Fx21+Fx22-(P+W2));...
-1/m2*((Cy21+Cy22)*q(8,1)+Fy21+Fy22)];
dq(1:4,1)=q(5:8,1); %????
主程序:
function Rotors_System_Func %???
clear
clc
global BN Nb1 Nb2 w1 w2 Ro1 Ri1 Ro2 Ri2 %????
n_one_T=200; %???????
n_T=100; %?????
Ro1=4.8828e-2; %??
Ri1=6.8672e-2;
Nb1=10; %???
Ro2=66.515e-3;
Ri2=58.5e-3; %??????
Nb2=34; %???
n_n=0; %????
w2_min=100; % ??
w2_max=10600;
w2_step=100; %??????
w1_rpm=11000; %W1??
q_initial(1:8,1)=1e-11; %?????
BN=Ri1/(Ri1+Ro1)*Nb1; %???????
tic
%w2_rpm=100;
for w2_rpm=w2_min:w2_step:w2_max
n_n=n_n+1
w2=w2_rpm/60;
w1=w1_rpm/60; %?????
r=Ro2/(Ro2+Ri2);
%w_cage_1=w1*r+w2*(1-r); %?????
%w_vc_1=w_cage_1*Nb2;
%T_vc_1=2*pi/w_vc_1;
w_cage=w2*BN;
w_vc=w_cage;
T_vc=2*pi/w_vc*n_n; %??
dt=T_vc/n_one_T; %????
%n_1=T_vc_1/dt;
time=n_T*T_vc; %???
n=round(time/dt); %????
t_span(1:n)=linspace(0,time,n);
%options=odeset('RelTol',1e-6);
%[t,q]=ode45('Rotors_System_Sub_Func',t_span,q_initial,options);
[t,q]=ode45('Rotors_System_Sub_Func',t_span,q_initial);
%subplot(2,2,1);plot(w2_rpm,q(8500:100:10000,5),'k.','markersize',5)
%hold on
plot(w2_rpm,q(15000:200:end,8),'k.','markersize',5)
hold on
%subplot(2,2,3);plot(w2_rpm,q(8500:100:10000,7),'k.','markersize',1)
%hold on
%subplot(2,2,4);plot(w2_rpm,q(8500:100:10000,8),'k.','markersize',1)
%hold on
end
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