Multi-variable fminsearch: Not enough input arguments
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I am getting 'Not enough input arguments' as result. Need help.
Function:
function qout = Lobo(d0, L, Tg, nb, uo)
clc
%Fuel flowrate
Ti = 251.9 + 273.15; %Fluid in degK
T0 = 386.1 + 273.15; %Fluid/gas out degK
cpL = 0.32; %Cp fluid KJ/kgdegK
flowL = 500; %flowrate fluid kg/s
THD = flowL.*cpL.*(T0 - Ti);%Total Heat Duty
Ef = 0.9320; %Fuel efficiency
qfuel = THD./Ef;%Heat released by fuel Kw
LHV = 41.05; %Fuel value KJ/kg
mfuel = qfuel./LHV;
%absorptivity
hp = 6.626*(10^-34); %planck's constant m2kg/s
cl = 3*(10^8); %speed of light m2/s
lamda = hp*cl/qfuel; %wavelength
Avog = 6.023*10^24; %Avogadro's number
x1 = 0.9;
M1 = 16;
x2 = 0.1;
M2 = 29;
fatmass = x1*M1 + x2*M2; %fuel molecular mass
nA = mfuel*Avog*fatmass; %number of atoms
pi = 22/7;
alpha = 4.*pi.*nA./lamda;
%Exchange factor
x = pi.*d0/2; %ctc
F = ((sqrt(x.^2 - 4) - x + 2.*sinh(2./x))/2.*pi);
%Heat transfer coefficient
k = 0.25*10^-3; %Thermal conductivity
%rof = 1320; %density
Gm = 920880; %mass flowrate
mu = 130; %Viscosity Pa-s
A0 = pi.*d0.*d0./4;
h0 = ((d0./k).*(0.023.*((Gm.*d0./mu.*A0).^0.8).*((cpL.*mu./k)).^0.3));
%Tube wall temperature
Tref = 41; %Ambient
Tw = Tref + (Ti - T0)/L;
%Air
ea = 0.15; %excess air
cpair = 0.171; %Kcal/kgdegK
Tairin = 114;
atfr = 1.344; %in notebook
mair = mfuel.*atfr.*(1+ea);
%Flame calculation
cpsteam = 4.1855;
cpco2 = 0.918;
cpn2 = 1.044;
xco2 = 0.054;
xsteam = 0.034; %Total should be 8.8
xn2 = 0.66;
cpgas = xsteam.*cpsteam + xco2.*cpco2 + xn2.*cpn2;
kgas = 0.25; %Thermal conductivity
mgas = mfuel + mair;
Lf = 0.0042.*(qfuel.^0.478); %flame length
tf = sqrt(pi.*uo.*Lf.*cpgas./mgas.*kgas); %flame size
db = 1.5.*tf; %Burner tile diameter
dbc = db./(sin(180./nb) + (pi./nb)); %Burner circle diameter
%Cold plane area
cbt = (qfuel.*1.055/4*10^6) + 1.5;
dtc = cbt + dbc; %tube circle diameter
ntubes = pi.*dtc./x;
Ar = L.*ntubes.*x;
%Radiant heat flux
stef = 5.67*10^-8; %Stefan-Boltzmann constant
qr = stef.*alpha.*F.*(Tg.^4 - Tw.^4) + ho.*(Tg - Tw);
%qr = stef*alpha*((sqrt((pi*d0)^2 - 16) - 2*x + 2*sinh(4/pi*d0))/4*pi)*(Tg^4 - (Tref + (Ti - T0)/L)^4) + ((d0/k)*(0.023*((Gm*d0/mu*pi*d0*d0/4)^0.8)*((cpL*mu/k))^0.3))*(Tg - (Tref + (Ti - T0)/L));
%Heat leaving
Qr = qr .* Ar; %total radiant heat absorbed
%Qr = qr * L*pi*(((qfuel*1.055/4*10^6) + 1.5) + ((1.5*(sqrt(pi*uo*Lf*cpgas/mgas*kgas)))/(sin(180/nb) + (pi/nb))));
qair = mair.*cpair.*(Tairin - Tref);
qloss = 0.05.*qfuel;
qout = qfuel + qair - ((stef.*alpha.*((sqrt((pi.*d0).^2 - 16) - 2.*x + 2*sinh(4/pi.*d0))/4*pi).*(Tg.^4 - (Tref + (Ti - T0)/L).^4) + ((d0/k).*(0.023.*((Gm.*d0/mu.*pi.*d0.*d0/4)^0.8).*((cpL.*mu./k)).^0.3)).*(Tg - (Tref + (Ti - T0)/L)).*L.*pi.*(((qfuel.*1.055/4*10^6) + 1.5) + ((1.5.*(sqrt(pi.*uo.*Lf.*cpgas./mgas.*kgas)))/(sin(180/nb) + (pi/nb))))) + qloss);
end
Solution:
%d0 = 0.01:1;
%L = 1:18;
%Tg = 1:1950;
%nb = 8:12;
%uo = 1:50;
x0 = [0.01, 1, 10, 8, 1];
options = optimset('PlotFcns',@optimplotfval);
X = fminsearch(@Lobo, x0, options);
qr = @Lobo;
plot (d0,qr)
xlabel('Tube circle diameter (d0)');
ylabel('flux (qr)');
Answers (1)
Walter Roberson
on 7 Mar 2018
X = fminsearch(@Lobo, x0, options);
invokes Lobo with one input vector which is the same length as x0.
You probably want
X = fminsearch(@(x) Lobo(x(1),x(2),x(3),x(4),x(5)), x0, options);
22 Comments
Devdatt Thengdi
on 7 Mar 2018
Devdatt Thengdi
on 7 Mar 2018
Devdatt Thengdi
on 8 Mar 2018
Devdatt Thengdi
on 8 Mar 2018
Devdatt Thengdi
on 8 Mar 2018
Torsten
on 8 Mar 2018
If you want to put constraints on some of your design variables, use "fmincon" instead of "fminsearch".
Best wishes
Torsten.
Devdatt Thengdi
on 8 Mar 2018
Walter Roberson
on 8 Mar 2018
fmincon, non-linear constraint function. qr can be calculated from the inputs so it can be constraint by a non-linear constraint function.
I suggest extracting all of the logic used to calculate qr into a function that you call from both the objective function and the nonlinear constraint function. This might involve calculating other variables as well in order to be able to calculate qr.
Torsten
on 8 Mar 2018
But qr is a function of the design variables, say qr = f(x1,...,x5), so you can constrain it by using the nonlinear constraint function of fmincon to set f(x1,...,x5) <= some value.
Devdatt Thengdi
on 8 Mar 2018
Devdatt Thengdi
on 8 Mar 2018
Torsten
on 8 Mar 2018
function [c,ceq] = nonlcon(d0, L, Tg, nb, uo)
%Fuel flowrate
Ti = 251.9 + 273.15; %Fluid in degK
T0 = 386.1 + 273.15; %Fluid/gas out degK
cpL = 0.32; %Cp fluid KJ/kgdegK
flowL = 500; %flowrate fluid kg/s
THD = flowL.*cpL.*(T0 - Ti);%Total Heat Duty
Ef = 0.9320; %Fuel efficiency
qfuel = THD./Ef;%Heat released by fuel Kw
LHV = 41.05; %Fuel value KJ/kg
mfuel = qfuel./LHV;
%absorptivity
hp = 6.626*(10^-34); %planck's constant m2kg/s
cl = 3*(10^8); %speed of light m2/s
lamda = hp*cl/qfuel; %wavelength
Avog = 6.023*10^24; %Avogadro's number
x1 = 0.9;
M1 = 16;
x2 = 0.1;
M2 = 29;
fatmass = x1*M1 + x2*M2; %fuel molecular mass
nA = mfuel*Avog*fatmass; %number of atoms
pi = 22/7;
alpha = 4.*pi.*nA./lamda;
%Exchange factor
x = pi.*d0/2; %ctc
F = ((sqrt(x.^2 - 4) - x + 2.*sinh(2./x))/2.*pi);
%Heat transfer coefficient
k = 0.25*10^-3; %Thermal conductivity
%rof = 1320; %density
Gm = 920880; %mass flowrate
mu = 130; %Viscosity Pa-s
A0 = pi.*d0.*d0./4;
h0 = ((d0./k).*(0.023.*((Gm.*d0./mu.*A0).^0.8).*((cpL.*mu./k)).^0.3));
%Tube wall temperature
Tref = 41; %Ambient
Tw = Tref + (Ti - T0)/L;
%Air
ea = 0.15; %excess air
cpair = 0.171; %Kcal/kgdegK
Tairin = 114;
atfr = 1.344; %in notebook
mair = mfuel.*atfr.*(1+ea);
%Flame calculation
cpsteam = 4.1855;
cpco2 = 0.918;
cpn2 = 1.044;
xco2 = 0.054;
xsteam = 0.034; %Total should be 8.8
xn2 = 0.66;
cpgas = xsteam.*cpsteam + xco2.*cpco2 + xn2.*cpn2;
kgas = 0.25; %Thermal conductivity
mgas = mfuel + mair;
Lf = 0.0042.*(qfuel.^0.478); %flame length
tf = sqrt(pi.*uo.*Lf.*cpgas./mgas.*kgas); %flame size
db = 1.5.*tf; %Burner tile diameter
dbc = db./(sin(180./nb) + (pi./nb)); %Burner circle diameter
%Cold plane area
cbt = (qfuel.*1.055/4*10^6) + 1.5;
dtc = cbt + dbc; %tube circle diameter
ntubes = pi.*dtc./x;
Ar = L.*ntubes.*x;
%Radiant heat flux
stef = 5.67*10^-8; %Stefan-Boltzmann constant
qr = stef.*alpha.*F.*(Tg.^4 - Tw.^4) + ho.*(Tg - Tw);
% Set constraints
ceq = [];
c(1) = qr - 45000; % qr <= 45000
c(2) = -qr + 32000; % qr >= 32000
end
Walter Roberson
on 8 Mar 2018
That code uses the undefined variable ho . Perhaps you mean h0 ?
In the line
cbt = (qfuel.*1.055/4*10^6) + 1.5;
could you verify that you want to take 1.055, divide by 4, and multiply the result by 10^6? Or did you want to divide by (4*10^6) ?
Why are you using
pi = 22/7
when more accurate versions are easily available?
Devdatt Thengdi
on 10 Mar 2018
Devdatt Thengdi
on 10 Mar 2018
Walter Roberson
on 10 Mar 2018
MATLAB predefines pi (lowercase, just like you used) to be the most accurate representation of π possible in double precision
Devdatt Thengdi
on 11 Mar 2018
Walter Roberson
on 11 Mar 2018
Your line
X = fmincon(@(x)Lobo(x(1),x(2),x(3),x(4),x(5)), x0, [], [], [], [], [], [], @(c)Lobo(c(1), c(2)), options);
tries to use your objective function, Lobo, as also being the nonlinear constraint function. But the nonlinear constraint function needs to have two outputs and Lobo only has one output, so you cannot use Lobo there. You should be calling your nonlcon in that position before options. And make sure you pass in all of the arguments that your nonlcon needs -- your anonymous function is only passing in the first two elements of the parameters but your nonlcon expects 5 inputs.
Devdatt Thengdi
on 13 Mar 2018
Torsten
on 13 Mar 2018
Set F=[F1,-F2] - then both functions F1 and F2 are to be minimized.
Best wishes
Torsten.
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