Add Matlab directory
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matlab/STEPS/00121403_defeature.STEP
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matlab/STEPS/00121403_defeature.STEP
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matlab/STEPS/00121413_defeature.STEP
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matlab/STEPS/00121413_defeature.STEP
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matlab/STEPS/12121142_defeature.STEP
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matlab/STEPS/12121142_defeature.STEP
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matlab/STEPS/12121147_defeature.STEP
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matlab/STEPS/12121147_defeature.STEP
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matlab/STEPS/nut_concave.STEP
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END-ISO-10303-21;
|
10006
matlab/STEPS/vionic_encoder.STEP
Normal file
10006
matlab/STEPS/vionic_encoder.STEP
Normal file
File diff suppressed because it is too large
Load Diff
105
matlab/src/initializeAPA.m
Normal file
105
matlab/src/initializeAPA.m
Normal file
@ -0,0 +1,105 @@
|
||||
function [actuator] = initializeAPA(args)
|
||||
% initializeAPA -
|
||||
%
|
||||
% Syntax: [actuator] = initializeAPA(args)
|
||||
%
|
||||
% Inputs:
|
||||
% - args -
|
||||
%
|
||||
% Outputs:
|
||||
% - actuator -
|
||||
|
||||
arguments
|
||||
args.type char {mustBeMember(args.type,{'2dof', 'flexible frame', 'flexible'})} = '2dof'
|
||||
|
||||
% Actuator and Sensor constants
|
||||
args.Ga (1,1) double {mustBeNumeric} = 0
|
||||
args.Gs (1,1) double {mustBeNumeric} = 0
|
||||
|
||||
% For 2DoF
|
||||
args.k (6,1) double {mustBeNumeric, mustBePositive} = ones(6,1)*0.38e6
|
||||
args.ke (6,1) double {mustBeNumeric, mustBePositive} = ones(6,1)*1.75e6
|
||||
args.ka (6,1) double {mustBeNumeric, mustBePositive} = ones(6,1)*3e7
|
||||
|
||||
args.c (6,1) double {mustBeNumeric, mustBePositive} = ones(6,1)*3e1
|
||||
args.ce (6,1) double {mustBeNumeric, mustBePositive} = ones(6,1)*2e1
|
||||
args.ca (6,1) double {mustBeNumeric, mustBePositive} = ones(6,1)*2e1
|
||||
|
||||
args.Leq (6,1) double {mustBeNumeric} = ones(6,1)*0.056
|
||||
|
||||
% Force Flexible APA
|
||||
args.xi (1,1) double {mustBeNumeric, mustBePositive} = 0.01
|
||||
args.d_align (3,1) double {mustBeNumeric} = zeros(3,1) % [m]
|
||||
args.d_align_bot (3,1) double {mustBeNumeric} = zeros(3,1) % [m]
|
||||
args.d_align_top (3,1) double {mustBeNumeric} = zeros(3,1) % [m]
|
||||
|
||||
% For Flexible Frame
|
||||
args.ks (1,1) double {mustBeNumeric, mustBePositive} = 235e6
|
||||
args.cs (1,1) double {mustBeNumeric, mustBePositive} = 1e1
|
||||
end
|
||||
|
||||
actuator = struct();
|
||||
|
||||
switch args.type
|
||||
case '2dof'
|
||||
actuator.type = 1;
|
||||
case 'flexible frame'
|
||||
actuator.type = 2;
|
||||
case 'flexible'
|
||||
actuator.type = 3;
|
||||
end
|
||||
|
||||
if args.Ga == 0
|
||||
switch args.type
|
||||
case '2dof'
|
||||
actuator.Ga = -30.0;
|
||||
case 'flexible frame'
|
||||
actuator.Ga = 1; % TODO
|
||||
case 'flexible'
|
||||
actuator.Ga = 23.4;
|
||||
end
|
||||
else
|
||||
actuator.Ga = args.Ga; % Actuator gain [N/V]
|
||||
end
|
||||
|
||||
if args.Gs == 0
|
||||
switch args.type
|
||||
case '2dof'
|
||||
actuator.Gs = 0.098;
|
||||
case 'flexible frame'
|
||||
actuator.Gs = 1; % TODO
|
||||
case 'flexible'
|
||||
actuator.Gs = -4674824;
|
||||
end
|
||||
else
|
||||
actuator.Gs = args.Gs; % Sensor gain [V/m]
|
||||
end
|
||||
|
||||
actuator.k = args.k; % [N/m]
|
||||
actuator.ke = args.ke; % [N/m]
|
||||
actuator.ka = args.ka; % [N/m]
|
||||
|
||||
actuator.c = args.c; % [N/(m/s)]
|
||||
actuator.ce = args.ce; % [N/(m/s)]
|
||||
actuator.ca = args.ca; % [N/(m/s)]
|
||||
|
||||
actuator.Leq = args.Leq; % [m]
|
||||
|
||||
switch args.type
|
||||
case 'flexible frame'
|
||||
actuator.K = readmatrix('APA300ML_b_mat_K.CSV'); % Stiffness Matrix
|
||||
actuator.M = readmatrix('APA300ML_b_mat_M.CSV'); % Mass Matrix
|
||||
actuator.P = extractNodes('APA300ML_b_out_nodes_3D.txt'); % Node coordinates [m]
|
||||
case 'flexible'
|
||||
actuator.K = readmatrix('full_APA300ML_K.CSV'); % Stiffness Matrix
|
||||
actuator.M = readmatrix('full_APA300ML_M.CSV'); % Mass Matrix
|
||||
actuator.P = extractNodes('full_APA300ML_out_nodes_3D.txt'); % Node coordiantes [m]
|
||||
actuator.d_align = args.d_align;
|
||||
actuator.d_align_bot = args.d_align_bot;
|
||||
actuator.d_align_top = args.d_align_top;
|
||||
end
|
||||
|
||||
actuator.xi = args.xi; % Damping ratio
|
||||
|
||||
actuator.ks = args.ks; % Stiffness of one stack [N/m]
|
||||
actuator.cs = args.cs; % Damping of one stack [N/m]
|
866
matlab/src/vectfit3.m
Normal file
866
matlab/src/vectfit3.m
Normal file
@ -0,0 +1,866 @@
|
||||
function [SER,poles,rmserr,fit,opts]=vectfit3(f,s,poles,weight,opts);
|
||||
%
|
||||
%function [SER,poles,rmserr,fit,opts]=vectfit3(f,s,poles,weight,opts)
|
||||
%function [SER,poles,rmserr,fit]=vectfit3(f,s,poles,weight,opts)
|
||||
%function [SER,poles,rmserr,fit]=vectfit3(f,s,poles,weight)
|
||||
%
|
||||
% ===========================================================
|
||||
% = Fast Relaxed Vector Fitting =
|
||||
% = Version 1.0 =
|
||||
% = Last revised: 08.08.2008 =
|
||||
% = Written by: Bjorn Gustavsen =
|
||||
% = SINTEF Energy Research, N-7465 Trondheim, NORWAY =
|
||||
% = bjorn.gustavsen@sintef.no =
|
||||
% = http://www.energy.sintef.no/Produkt/VECTFIT/index.asp =
|
||||
% = Note: RESTRICTED to NON-COMMERCIAL use =
|
||||
% ===========================================================
|
||||
%
|
||||
% PURPOSE : Approximate f(s) with a state-space model
|
||||
%
|
||||
% f(s)=C*(s*I-A)^(-1)*B +D +s*E
|
||||
%
|
||||
% where f(s) is a singe element or a vector of elements.
|
||||
% When f(s) is a vector, all elements become fitted with a common
|
||||
% pole set.
|
||||
%
|
||||
% INPUT :
|
||||
%
|
||||
% f(s) : function (vector) to be fitted.
|
||||
% dimension : (Nc,Ns)
|
||||
% Nc : number of elements in vector
|
||||
% Ns : number of frequency samples
|
||||
%
|
||||
% s : vector of frequency points [rad/sec]
|
||||
% dimension : (1,Ns)
|
||||
%
|
||||
% poles : vector of initial poles [rad/sec]
|
||||
% dimension : (1,N)
|
||||
%
|
||||
% weight: the rows in the system matrix are weighted using this array. Can be used
|
||||
% for achieving higher accuracy at desired frequency samples.
|
||||
% If no weighting is desired, use unitary weights: weight=ones(1,Ns).
|
||||
%
|
||||
% Two dimensions are allowed:
|
||||
% dimension : (1,Ns) --> Common weighting for all vector elements.
|
||||
% dimension : (Nc,Ns)--> Individual weighting for vector elements.
|
||||
%
|
||||
% opts.relax==1 --> Use relaxed nontriviality constraint
|
||||
% opts.relax==0 --> Use nontriviality constraint of "standard" vector fitting
|
||||
%
|
||||
% opts.stable=0 --> unstable poles are kept unchanged
|
||||
% opts.stable=1 --> unstable poles are made stable by 'flipping' them
|
||||
% into the left half-plane
|
||||
%
|
||||
%
|
||||
% opts.asymp=1 --> Fitting with D=0, E=0
|
||||
% opts.asymp=2 --> Fitting with D~=0, E=0
|
||||
% opts.asymp=3 --> Fitting with D~=0, E~=0
|
||||
%
|
||||
% opts.spy1=1 --> Plotting, after pole identification (A)
|
||||
% figure(3): magnitude functions
|
||||
% cyan trace : (sigma*f)fit
|
||||
% red trace : (sigma)fit
|
||||
% green trace : f*(sigma)fit - (sigma*f)fit
|
||||
%
|
||||
% opts.spy2=1 --> Plotting, after residue identification (C,D,E)
|
||||
% figure(1): magnitude functions
|
||||
% figure(2): phase angles
|
||||
%
|
||||
% opts.logx=1 --> Plotting using logarithmic absissa axis
|
||||
%
|
||||
% opts.logy=1 --> Plotting using logarithmic ordinate axis
|
||||
%
|
||||
% opts.errplot=1 --> Include deviation in magnitude plot
|
||||
%
|
||||
% opts.phaseplot=1 -->Show plot also for phase angle
|
||||
%
|
||||
%
|
||||
% opts.skip_pole=1 --> The pole identification part is skipped, i.e (C,D,E)
|
||||
% are identified using the initial poles (A) as final poles.
|
||||
%
|
||||
% opts.skip_res =1 --> The residue identification part is skipped, i.e. only the
|
||||
% poles (A) are identified while C,D,E are returned as zero.
|
||||
%
|
||||
%
|
||||
% opts.cmplx_ss =1 -->The returned state-space model has real and complex conjugate
|
||||
% parameters. Output variable A is diagonal (and sparse).
|
||||
% =0 -->The returned state-space model has real parameters only.
|
||||
% Output variable A is square with 2x2 blocks (and sparse).
|
||||
%
|
||||
% OUTPUT :
|
||||
%
|
||||
% fit(s) = C*(s*I-(A)^(-1)*B +D +s.*E
|
||||
%
|
||||
% SER.A(N,N) : A-matrix (sparse). If cmplx_ss==1: Diagonal and complex.
|
||||
% Otherwise, square and real with 2x2 blocks.
|
||||
%
|
||||
% SER.B(N,1) : B-matrix. If cmplx_ss=1: Column of 1's.
|
||||
% If cmplx_ss=0: contains 0's, 1's and 2's)
|
||||
% SER.C(Nc,N) : C-matrix. If cmplx_ss=1: complex
|
||||
% If cmplx_ss=0: real-only
|
||||
% SERD.D(Nc,1) : constant term (real). Is non-zero if asymp=2 or 3.
|
||||
% SERE.E(Nc,1) : proportional term (real). Is non-zero if asymp=3.
|
||||
%
|
||||
% poles(1,N) : new poles
|
||||
%
|
||||
% rmserr(1) : root-mean-square error of approximation for f(s).
|
||||
% (0 is returned if skip_res==1)
|
||||
% fit(Nc,Ns): Rational approximation at samples. (0 is returned if
|
||||
% skip_res==1).
|
||||
%
|
||||
%
|
||||
% APPROACH:
|
||||
% The identification is done using the pole relocating method known as Vector Fitting [1],
|
||||
% with relaxed non-triviality constraint for faster convergence and smaller fitting errors [2],
|
||||
% and utilization of matrix structure for fast solution of the pole identifion step [3].
|
||||
%
|
||||
%********************************************************************************
|
||||
% NOTE: The use of this program is limited to NON-COMMERCIAL usage only.
|
||||
% If the program code (or a modified version) is used in a scientific work,
|
||||
% then reference should be made to the following:
|
||||
%
|
||||
% [1] B. Gustavsen and A. Semlyen, "Rational approximation of frequency
|
||||
% domain responses by Vector Fitting", IEEE Trans. Power Delivery,
|
||||
% vol. 14, no. 3, pp. 1052-1061, July 1999.
|
||||
%
|
||||
% [2] B. Gustavsen, "Improving the pole relocating properties of vector
|
||||
% fitting", IEEE Trans. Power Delivery, vol. 21, no. 3, pp. 1587-1592,
|
||||
% July 2006.
|
||||
%
|
||||
% [3] D. Deschrijver, M. Mrozowski, T. Dhaene, and D. De Zutter,
|
||||
% "Macromodeling of Multiport Systems Using a Fast Implementation of
|
||||
% the Vector Fitting Method", IEEE Microwave and Wireless Components
|
||||
% Letters, vol. 18, no. 6, pp. 383-385, June 2008.
|
||||
%********************************************************************************
|
||||
% This example script is part of the vector fitting package (VFIT3.zip)
|
||||
% Last revised: 08.08.2008.
|
||||
% Created by: Bjorn Gustavsen.
|
||||
%
|
||||
%
|
||||
def.relax=1; %Use vector fitting with relaxed non-triviality constraint
|
||||
def.stable=1; %Enforce stable poles
|
||||
def.asymp=2; %Include only D in fitting (not E)
|
||||
def.skip_pole=0; %Do NOT skip pole identification
|
||||
def.skip_res=0; %Do NOT skip identification of residues (C,D,E)
|
||||
def.cmplx_ss=1; %Create complex state space model
|
||||
def.spy1=0; %No plotting for first stage of vector fitting
|
||||
def.spy2=1; %Create magnitude plot for fitting of f(s)
|
||||
def.logx=1; %Use logarithmic abscissa axis
|
||||
def.logy=1; %Use logarithmic ordinate axis
|
||||
def.errplot=1; %Include deviation in magnitude plot
|
||||
def.phaseplot=0; %exclude plot of phase angle (in addition to magnitiude)
|
||||
def.legend=1; %Do include legends in plots
|
||||
|
||||
|
||||
if nargin<5
|
||||
opts=def;
|
||||
else
|
||||
%Merge default values into opts
|
||||
A=fieldnames(def);
|
||||
for m=1:length(A)
|
||||
if ~isfield(opts,A(m))
|
||||
dum=char(A(m)); dum2=getfield(def,dum); opts=setfield(opts,dum,dum2);
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
|
||||
|
||||
%Tolerances used by relaxed version of vector fitting
|
||||
TOLlow=1e-18; TOLhigh=1e18;
|
||||
|
||||
[a,b]=size(poles);
|
||||
if s(1)==0 && a==1
|
||||
if poles(1)==0 && poles(2)~=0
|
||||
poles(1)=-1;
|
||||
elseif poles(2)==0 && poles(1)~=0
|
||||
poles(2)=-1;
|
||||
elseif poles(1)==0 && poles(2)==0
|
||||
poles(1)=-1+i*10; poles(2)=-1-i*10;
|
||||
end
|
||||
end
|
||||
|
||||
if (opts.relax~=0) && (opts.relax)~=1
|
||||
disp([' ERROR in vectfit3.m: ==> Illegal value for opts.relax: ' num2str(opts.asymp)]),return
|
||||
end
|
||||
if (opts.asymp~=1) && (opts.asymp)~=2 && (opts.asymp)~=3
|
||||
disp([' ERROR in vectfit3.m: ==> Illegal value for opts.asymp: ' num2str(opts.asymp)]),return
|
||||
end
|
||||
if (opts.stable~=0) && (opts.stable~=1)
|
||||
disp([' ERROR in vectfit3.m: ==> Illegal value for opts.stable: ' num2str(opts.stable)]),return
|
||||
end
|
||||
if (opts.skip_pole~=0) && (opts.skip_pole)~=1
|
||||
disp([' ERROR in vectfit3.m: ==> Illegal value for opts.skip_pole: ' num2str(opts.skip_pole)]),return
|
||||
end
|
||||
if (opts.skip_res~=0) && (opts.skip_res)~=1
|
||||
disp([' ERROR in vectfit3.m: ==> Illegal value for opts.skip_res: ' num2str(opts.skip_res)]),return
|
||||
end
|
||||
if (opts.cmplx_ss~=0) && (opts.cmplx_ss)~=1
|
||||
disp([' ERROR in vectfit3.m: ==> Illegal value for opts.cmplx_ss: ' num2str(opts.cmplx_ss)]),return
|
||||
end
|
||||
|
||||
rmserr=[];%SERC=[];
|
||||
[a,b]=size(s);
|
||||
if a<b, s=s.'; end
|
||||
|
||||
% Some sanity checks on dimension of input arrays:
|
||||
if length(s)~=length(f(1,:))
|
||||
disp('Error in vectfit3.m!!! ==> Second dimension of f does not match length of s.');
|
||||
return;
|
||||
end
|
||||
if length(s)~=length(weight(1,:))
|
||||
disp('Error in vectfit3.m!!! ==> Second dimension of weight does not match length of s.');
|
||||
return;
|
||||
end
|
||||
if length(weight(:,1))~=1
|
||||
if length(weight(:,1))~=length(f(:,1))
|
||||
disp('Error in vectfit3.m!!! ==> First dimension of weight is neither 1 nor matches first dimension of f.');
|
||||
return;
|
||||
end
|
||||
end
|
||||
|
||||
%set(0,'DefaultLineLineWidth',0.5) ; set(0,'DefaultLineMarkerSize',4) ;
|
||||
%clear b; clear C;
|
||||
LAMBD=diag(poles);
|
||||
Ns=length(s); N=length(LAMBD); Nc=length(f(:,1));
|
||||
B=ones(N,1); %I=diag(ones(1,N));
|
||||
SERA=poles;SERC=zeros(Nc,N);SERD=zeros(Nc,1);SERE=zeros(Nc,1);
|
||||
roetter=poles;
|
||||
fit=zeros(Nc,Ns);
|
||||
|
||||
weight=weight.';
|
||||
if length(weight(1,:))==1
|
||||
common_weight=1;
|
||||
elseif length(weight(1,:))==Nc
|
||||
common_weight=0;
|
||||
else
|
||||
disp('ERROR in vectfit3.m: Invalid size of array weight')
|
||||
return
|
||||
end
|
||||
|
||||
if opts.asymp==1
|
||||
offs=0;
|
||||
elseif opts.asymp==2
|
||||
offs=1;
|
||||
else
|
||||
offs=2;
|
||||
end
|
||||
|
||||
|
||||
|
||||
%=========================================================================
|
||||
%=========================================================================
|
||||
% POLE IDENTIFICATION:
|
||||
%=========================================================================
|
||||
%=========================================================================
|
||||
|
||||
|
||||
if opts.skip_pole~=1
|
||||
|
||||
|
||||
|
||||
Escale=zeros(1,Nc+1);
|
||||
|
||||
|
||||
%=======================================================
|
||||
% Finding out which starting poles are complex :
|
||||
%=======================================================
|
||||
cindex=zeros(1,N);
|
||||
for m=1:N
|
||||
if imag(LAMBD(m,m))~=0
|
||||
if m==1
|
||||
cindex(m)=1;
|
||||
else
|
||||
if cindex(m-1)==0 || cindex(m-1)==2
|
||||
cindex(m)=1; cindex(m+1)=2;
|
||||
else
|
||||
cindex(m)=2;
|
||||
end
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
%=======================================================
|
||||
% Building system - matrix :
|
||||
%=======================================================
|
||||
%I3=diag(ones(1,Nc));I3(:,Nc)=[];
|
||||
Dk=zeros(Ns,N);
|
||||
for m=1:N
|
||||
if cindex(m)==0 %real pole
|
||||
Dk(:,m)=1./(s-LAMBD(m,m));
|
||||
elseif cindex(m)==1 %complex pole, 1st part
|
||||
Dk(:,m) =1./(s-LAMBD(m,m)) + 1./(s-LAMBD(m,m)');
|
||||
Dk(:,m+1)=i./(s-LAMBD(m,m)) - i./(s-LAMBD(m,m)');
|
||||
end
|
||||
end
|
||||
if opts.asymp==1 || opts.asymp==2
|
||||
Dk(:,N+1)=1;
|
||||
elseif opts.asymp==3
|
||||
Dk(:,N+1)=1;
|
||||
Dk(:,N+2)=s;
|
||||
end
|
||||
|
||||
%Scaling for last row of LS-problem (pole identification)
|
||||
scale=0;
|
||||
for m=1:Nc
|
||||
if length(weight(1,:))==1
|
||||
scale=scale+(norm(weight(:,1).*f(m,:).'))^2;
|
||||
else
|
||||
scale=scale+(norm(weight(:,m).*f(m,:).'))^2;
|
||||
end
|
||||
end
|
||||
scale=sqrt(scale)/Ns;
|
||||
|
||||
|
||||
if opts.relax==1
|
||||
|
||||
%Escale=zeros(1,Nc*(N+offs)+N+1);
|
||||
%scale=norm(f);%/Ns; %Scaling for sigma in LS problem
|
||||
AA=zeros(Nc*(N+1),N+1);
|
||||
bb=zeros(Nc*(N+1),1);
|
||||
Escale=zeros(1,length(AA(1,:)));
|
||||
for n=1:Nc
|
||||
A=zeros(Ns,(N+offs) +N+1); %b=zeros(Ns*Nc+1,1);
|
||||
|
||||
if common_weight==1
|
||||
weig=weight;
|
||||
else
|
||||
weig=weight(:,n);
|
||||
end
|
||||
|
||||
|
||||
for m=1:N+offs %left block
|
||||
A(1:Ns,m)=weig.*Dk(1:Ns,m);
|
||||
end
|
||||
inda=N+offs;
|
||||
for m=1:N+1 %right block
|
||||
A(1:Ns,inda+m)=-weig.*Dk(1:Ns,m).*f(n,1:Ns).';
|
||||
end
|
||||
|
||||
A=[real(A);imag(A)];
|
||||
|
||||
|
||||
%Integral criterion for sigma:
|
||||
offset=(N+offs);
|
||||
if n==Nc
|
||||
for mm=1:N+1
|
||||
A(2*Ns+1,offset+mm)=real(scale*sum(Dk(:,mm)));
|
||||
end
|
||||
end
|
||||
[Q,R]=qr(A,0);
|
||||
ind1=N+offs+1;
|
||||
ind2=N+offs+N+1;
|
||||
R22=R(ind1:ind2,ind1:ind2);
|
||||
AA((n-1)*(N+1)+1:n*(N+1),:)=R22;
|
||||
if n==Nc
|
||||
bb((n-1)*(N+1)+1:n*(N+1),1)=Q(end,N+offs+1:end)'*Ns*scale;
|
||||
end
|
||||
end %for n=1:Nc
|
||||
|
||||
for col=1:length(AA(1,:))
|
||||
Escale(col)=1/norm(AA(:,col));
|
||||
AA(:,col)=Escale(col).*AA(:,col);
|
||||
end
|
||||
x=AA\bb;
|
||||
%size(x),size(Escale)
|
||||
x=x.*Escale.';
|
||||
|
||||
end %if opts.relax==0
|
||||
|
||||
|
||||
%Situation: No relaxation, or produced D of sigma extremely small and large. Solve again, without relaxation
|
||||
if opts.relax==0 | abs(x(end))<TOLlow | abs(x(end))>TOLhigh
|
||||
AA=zeros(Nc*(N),N);
|
||||
bb=zeros(Nc*(N),1);
|
||||
if opts.relax==0
|
||||
Dnew=1;
|
||||
else
|
||||
if x(end)==0
|
||||
Dnew=1;
|
||||
elseif abs(x(end))<TOLlow
|
||||
Dnew=sign(x(end))*TOLlow
|
||||
elseif abs(x(end))>TOLhigh
|
||||
Dnew=sign(x(end))*TOLhigh
|
||||
end
|
||||
end
|
||||
|
||||
for n=1:Nc
|
||||
A=zeros(Ns,(N+offs) +N); %b=zeros(Ns*Nc+1,1);
|
||||
Escale=zeros(1,N);
|
||||
|
||||
if common_weight==1
|
||||
weig=weight;
|
||||
else
|
||||
weig=weight(:,n);
|
||||
end
|
||||
|
||||
for m=1:N+offs %left block
|
||||
A(1:Ns,m)=weig.*Dk(1:Ns,m);
|
||||
end
|
||||
inda=N+offs;
|
||||
for m=1:N %right block
|
||||
A(1:Ns,inda+m)=-weig.*Dk(1:Ns,m).*f(n,1:Ns).';
|
||||
end
|
||||
b=Dnew*weig.*f(n,1:Ns).';
|
||||
A=[real(A);imag(A)];
|
||||
b=[real(b);imag(b)];
|
||||
offset=(N+offs);
|
||||
[Q,R]=qr(A,0);
|
||||
ind1=N+offs+1;
|
||||
ind2=N+offs+N;
|
||||
R22=R(ind1:ind2,ind1:ind2);
|
||||
AA((n-1)*N+1:n*N,:)=R22;
|
||||
bb((n-1)*N+1:n*N,1)=Q(:,ind1:ind2).'*b;
|
||||
end %for n=1:Nc
|
||||
for col=1:length(AA(1,:))
|
||||
Escale(col)=1./norm(AA(:,col));
|
||||
AA(:,col)=Escale(col).*AA(:,col);
|
||||
end
|
||||
|
||||
%if opts.use_normal==1
|
||||
% x=AA.'*AA\(AA.'*bb);
|
||||
%else
|
||||
x=AA\bb;
|
||||
%end
|
||||
x=x.*Escale.';
|
||||
x=[x;Dnew];
|
||||
|
||||
end %if opts.relax==0 | abs(x(end))<TOLlow | abs(x(end))>TOLhigh
|
||||
|
||||
|
||||
%************************************
|
||||
|
||||
C=x(1:end-1);
|
||||
D=x(end); %NEW!!
|
||||
|
||||
%We now change back to make C complex :
|
||||
% **************
|
||||
for m=1:N
|
||||
if cindex(m)==1
|
||||
for n=1:1%Nc+1
|
||||
r1=C(m); r2=C(m+1);
|
||||
C(m)=r1+i*r2; C(m+1)=r1-i*r2;
|
||||
end
|
||||
end
|
||||
end
|
||||
% **************
|
||||
|
||||
if opts.spy1==1
|
||||
Dk=zeros(Ns,N);
|
||||
for m=1:N
|
||||
Dk(:,m)=1./(s-LAMBD(m,m));
|
||||
end
|
||||
RES3(:,1)=D+Dk*C; % (sigma)rat
|
||||
freq=s./(2*pi*i);
|
||||
if opts.logx==1
|
||||
if opts.logy==1
|
||||
figure(3),
|
||||
h1=loglog(freq,abs(RES3'),'b'); xlim([freq(1) freq(Ns)]); %sigma*f
|
||||
else %logy=0
|
||||
figure(3),
|
||||
h1=semilogx(freq,abs(RES3'),'b'); xlim([freq(1) freq(Ns)]);
|
||||
end
|
||||
else %logx=0
|
||||
if opts.logy==1
|
||||
figure(3),
|
||||
h1=semilogy(freq,abs(RES3'),'b'); xlim([freq(1) freq(Ns)]);
|
||||
else %logy=0
|
||||
figure(3),
|
||||
h1=plot(s./(2*pi*i),abs(RES3'),'b'); xlim([freq(1) freq(Ns)]);
|
||||
end
|
||||
end
|
||||
figure(3),xlabel('Frequency [Hz]'); ylabel('Magnitude');
|
||||
%figure(3), title('Sigma')
|
||||
if opts.legend==1
|
||||
legend([h1(1)],'sigma');
|
||||
end
|
||||
drawnow;
|
||||
end
|
||||
|
||||
%=============================================================================
|
||||
% We now calculate the zeros for sigma :
|
||||
%=============================================================================
|
||||
%oldLAMBD=LAMBD;oldB=B;oldC=C;
|
||||
m=0;
|
||||
for n=1:N
|
||||
m=m+1;
|
||||
if m<N
|
||||
if( abs(LAMBD(m,m))>abs(real(LAMBD(m,m))) ) %complex number?
|
||||
LAMBD(m+1,m)=-imag(LAMBD(m,m)); LAMBD(m,m+1)=imag(LAMBD(m,m));
|
||||
LAMBD(m,m)=real(LAMBD(m,m));LAMBD(m+1,m+1)=LAMBD(m,m);
|
||||
B(m,1)=2; B(m+1,1)=0;
|
||||
koko=C(m); C(m)=real(koko); C(m+1)=imag(koko);
|
||||
m=m+1;
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
ZER=LAMBD-B*C.'/D;
|
||||
roetter=eig(ZER).';
|
||||
unstables=real(roetter)>0;
|
||||
if opts.stable==1
|
||||
roetter(unstables)=roetter(unstables)-2*real(roetter(unstables)); %Forcing unstable poles to be stable...
|
||||
end
|
||||
roetter=sort(roetter); N=length(roetter);
|
||||
|
||||
|
||||
%=============================================
|
||||
%Sorterer polene s.a. de reelle kommer først:
|
||||
for n=1:N
|
||||
for m=n+1:N
|
||||
if imag(roetter(m))==0 && imag(roetter(n))~=0
|
||||
trans=roetter(n); roetter(n)=roetter(m); roetter(m)=trans;
|
||||
end
|
||||
end
|
||||
end
|
||||
N1=0;
|
||||
for m=1:N
|
||||
if imag(roetter(m))==0, N1=m; end
|
||||
end
|
||||
if N1<N, roetter(N1+1:N)=sort(roetter(N1+1:N)); end % N1: n.o. real poles
|
||||
%N2=N-N1; % N2: n.o. imag.poles
|
||||
|
||||
roetter=roetter-2*i*imag(roetter); %10.11.97 !!!
|
||||
SERA=roetter.';
|
||||
|
||||
|
||||
end %if skip_pole~=1
|
||||
|
||||
%=========================================================================
|
||||
%=========================================================================
|
||||
% RESIDUE IDENTIFICATION:
|
||||
%=========================================================================
|
||||
%=========================================================================
|
||||
|
||||
if opts.skip_res~=1
|
||||
|
||||
%=============================================================================
|
||||
% We now calculate SER for f, using the modified zeros of sigma as new poles :
|
||||
%========================================================================================
|
||||
|
||||
%clear LAMBD A A1 xA1 xxA1 A2 xA2 xxA2 b xb xxb C RES1 RES2;
|
||||
|
||||
LAMBD=roetter;
|
||||
|
||||
%B=ones(N,1);
|
||||
|
||||
% Finding out which poles are complex :
|
||||
cindex=zeros(1,N);
|
||||
for m=1:N
|
||||
if imag(LAMBD(m))~=0
|
||||
if m==1
|
||||
cindex(m)=1;
|
||||
else
|
||||
if cindex(m-1)==0 || cindex(m-1)==2
|
||||
cindex(m)=1; cindex(m+1)=2;
|
||||
else
|
||||
cindex(m)=2;
|
||||
end
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
|
||||
%===============================================================================
|
||||
% We now calculate the SER for f (new fitting), using the above calculated
|
||||
% zeros as known poles :
|
||||
%===============================================================================
|
||||
if opts.asymp==1
|
||||
A=zeros(2*Ns,N); BB=zeros(2*Ns,Nc);
|
||||
elseif opts.asymp==2
|
||||
A=zeros(2*Ns,N+1); BB=zeros(2*Ns,Nc);
|
||||
else
|
||||
A=zeros(2*Ns,N+2); BB=zeros(2*Ns,Nc);
|
||||
end
|
||||
|
||||
%I3=diag(ones(1,Nc));I3(:,Nc)=[];
|
||||
Dk=zeros(Ns,N);
|
||||
for m=1:N
|
||||
if cindex(m)==0 %real pole
|
||||
Dk(:,m)=1./(s-LAMBD(m));
|
||||
elseif cindex(m)==1 %complex pole, 1st part
|
||||
Dk(:,m) =1./(s-LAMBD(m)) + 1./(s-LAMBD(m)');
|
||||
Dk(:,m+1)=i./(s-LAMBD(m)) - i./(s-LAMBD(m)');
|
||||
end
|
||||
end
|
||||
|
||||
|
||||
if common_weight==1
|
||||
|
||||
%I3=diag(ones(1,Nc));I3(:,Nc)=[];
|
||||
Dk=zeros(Ns,N);
|
||||
for m=1:N
|
||||
if cindex(m)==0 %real pole
|
||||
Dk(:,m)=weight./(s-LAMBD(m));
|
||||
elseif cindex(m)==1 %complex pole, 1st part
|
||||
Dk(:,m) =weight./(s-LAMBD(m)) + weight./(s-LAMBD(m)');
|
||||
Dk(:,m+1)=i.*weight./(s-LAMBD(m)) - i.*weight./(s-LAMBD(m)');
|
||||
end
|
||||
end
|
||||
|
||||
if opts.asymp==1
|
||||
A(1:Ns,1:N)=Dk;
|
||||
elseif opts.asymp==2
|
||||
A(1:Ns,1:N)=Dk; A(1:Ns,N+1)=weight;
|
||||
else
|
||||
A(1:Ns,1:N)=Dk; A(1:Ns,N+1)=weight; A(1:Ns,N+2)=weight.*s;
|
||||
end
|
||||
for m=1:Nc
|
||||
BB(1:Ns,m)=weight.*f(m,:).';
|
||||
end
|
||||
A(Ns+1:2*Ns,:)=imag(A(1:Ns,:));
|
||||
A(1:Ns,:)=real(A(1:Ns,:));
|
||||
BB(Ns+1:2*Ns,:)=imag(BB(1:Ns,:));
|
||||
BB(1:Ns,:)=real(BB(1:Ns,:));
|
||||
|
||||
if opts.asymp==2
|
||||
A(1:Ns,N+1)=A(1:Ns,N+1);
|
||||
elseif opts.asymp==3
|
||||
A(1:Ns,N+1)=A(1:Ns,N+1);
|
||||
A(Ns+1:2*Ns,N+2)=A(Ns+1:2*Ns,N+2);
|
||||
end
|
||||
|
||||
%clear Escale;
|
||||
Escale=zeros(1,length(A(1,:)));
|
||||
for col=1:length(A(1,:));
|
||||
Escale(col)=norm(A(:,col),2);
|
||||
A(:,col)=A(:,col)./Escale(col);
|
||||
end
|
||||
X=A\BB;
|
||||
for n=1:Nc
|
||||
X(:,n)=X(:,n)./Escale.';
|
||||
end
|
||||
|
||||
%clear A;
|
||||
X=X.';
|
||||
C=X(:,1:N);
|
||||
if opts.asymp==2
|
||||
SERD=X(:,N+1);
|
||||
elseif opts.asymp==3
|
||||
SERE=X(:,N+2);
|
||||
SERD=X(:,N+1);
|
||||
end
|
||||
|
||||
else %if common_weight==1
|
||||
|
||||
SERD=zeros(Nc,1);
|
||||
SERE=zeros(Nc,1);
|
||||
C=zeros(Nc,N);
|
||||
for n=1:Nc
|
||||
|
||||
if opts.asymp==1
|
||||
A(1:Ns,1:N)=Dk;
|
||||
elseif opts.asymp==2
|
||||
A(1:Ns,1:N)=Dk; A(1:Ns,N+1)=1;
|
||||
else
|
||||
A(1:Ns,1:N)=Dk; A(1:Ns,N+1)=1; A(1:Ns,N+2)=s;
|
||||
end
|
||||
|
||||
for m=1:length(A(1,:))
|
||||
A(1:Ns,m)=weight(:,n).*A(1:Ns,m);
|
||||
end
|
||||
|
||||
BB=weight(:,n).*f(n,:).';
|
||||
A(Ns+1:2*Ns,:)=imag(A(1:Ns,:));
|
||||
A(1:Ns,:)=real(A(1:Ns,:));
|
||||
BB(Ns+1:2*Ns)=imag(BB(1:Ns));
|
||||
BB(1:Ns)=real(BB(1:Ns));
|
||||
|
||||
if opts.asymp==2
|
||||
A(1:Ns,N+1)=A(1:Ns,N+1);
|
||||
elseif opts.asymp==3
|
||||
A(1:Ns,N+1)=A(1:Ns,N+1);
|
||||
A(Ns+1:2*Ns,N+2)=A(Ns+1:2*Ns,N+2);
|
||||
end
|
||||
|
||||
%clear Escale;
|
||||
Escale=zeros(1,length(A(1,:)));
|
||||
for col=1:length(A(1,:));
|
||||
Escale(col)=norm(A(:,col),2);
|
||||
A(:,col)=A(:,col)./Escale(col);
|
||||
end
|
||||
x=A\BB;
|
||||
x=x./Escale.';
|
||||
|
||||
%clear A;
|
||||
C(n,1:N)=x(1:N).';
|
||||
|
||||
if opts.asymp==2
|
||||
SERD(n)=x(N+1);
|
||||
elseif opts.asymp==3
|
||||
SERE(n)=x(N+2);
|
||||
SERD(n)=x(N+1);
|
||||
end
|
||||
|
||||
|
||||
end %for n=1:Nc
|
||||
|
||||
|
||||
end %if common_weight==1
|
||||
|
||||
|
||||
%=========================================================================
|
||||
|
||||
%We now change back to make C complex.
|
||||
for m=1:N
|
||||
if cindex(m)==1
|
||||
for n=1:Nc
|
||||
r1=C(n,m); r2=C(n,m+1);
|
||||
C(n,m)=r1+i*r2; C(n,m+1)=r1-i*r2;
|
||||
end
|
||||
end
|
||||
end
|
||||
% **************
|
||||
|
||||
|
||||
B=ones(N,1);
|
||||
|
||||
%====================================================
|
||||
|
||||
SERA = LAMBD;
|
||||
SERB = B;
|
||||
SERC = C;
|
||||
|
||||
|
||||
|
||||
Dk=zeros(Ns,N);
|
||||
for m=1:N
|
||||
Dk(:,m)=1./(s-SERA(m));
|
||||
end
|
||||
for n=1:Nc
|
||||
fit(n,:)=(Dk*SERC(n,:).').';
|
||||
if opts.asymp==2
|
||||
fit(n,:)=fit(n,:)+SERD(n);
|
||||
elseif opts.asymp==3
|
||||
fit(n,:)=fit(n,:)+SERD(n)+s.'.*SERE(n);
|
||||
end
|
||||
end
|
||||
|
||||
fit=fit.'; f=f.';
|
||||
diff=fit-f; rmserr=sqrt(sum(sum(abs(diff.^2))))/sqrt(Nc*Ns);
|
||||
|
||||
if opts.spy2==1
|
||||
freq=s./(2*pi*i);
|
||||
if opts.logx==1
|
||||
if opts.logy==1
|
||||
figure(1),
|
||||
h1=loglog(freq,abs(f),'b'); xlim([freq(1) freq(Ns)]);hold on
|
||||
h2=loglog(freq,abs(fit),'r--'); hold off
|
||||
if opts.errplot== 1
|
||||
hold on,h3=loglog(freq,abs(f-fit),'g');hold off;
|
||||
end
|
||||
else %logy=0
|
||||
figure(1),
|
||||
h1=semilogx(freq,abs(f),'b'); xlim([freq(1) freq(Ns)]);hold on
|
||||
h2=semilogx(freq,abs(fit),'r--'); hold off
|
||||
if opts.errplot== 1
|
||||
hold on,h3=semilogx(freq,abs(f-fit),'g');hold off;
|
||||
end
|
||||
end
|
||||
if opts.phaseplot==1
|
||||
figure(2),
|
||||
h4=semilogx(freq,180*unwrap(angle(f))/pi,'b'); xlim([freq(1) freq(Ns)]);hold on
|
||||
h5=semilogx(freq,180*unwrap(angle(fit))/pi,'r--');hold off
|
||||
end
|
||||
else %logx=0
|
||||
if opts.logy==1
|
||||
figure(1),
|
||||
h1=semilogy(freq,abs(f),'b'); xlim([freq(1) freq(Ns)]);hold on
|
||||
h2=semilogy(freq,abs(fit),'r--'); hold off
|
||||
if opts.errplot== 1
|
||||
hold on,h3=semilogy(freq,abs(f-fit),'g');hold off;
|
||||
end
|
||||
else %logy=0
|
||||
figure(1),
|
||||
h1=plot(freq,abs(f),'b'); xlim([freq(1) freq(Ns)]);hold on
|
||||
h2=plot(freq,abs(fit),'r--'); hold off
|
||||
if opts.errplot== 1
|
||||
hold on,h3=plot(freq,abs(f-fit),'g');hold off;
|
||||
end
|
||||
end
|
||||
if opts.phaseplot==1
|
||||
figure(2),
|
||||
h4=plot(freq,180*unwrap(angle(f))/pi,'b'); xlim([freq(1) freq(Ns)]);hold on
|
||||
h5=plot(freq,180*unwrap(angle(fit))/pi,'r--');hold off
|
||||
end
|
||||
end %logy=0
|
||||
figure(1),
|
||||
xlabel('Frequency [Hz]'); ylabel('Magnitude');
|
||||
%title('Approximation of f');
|
||||
if opts.legend==1
|
||||
if opts.errplot==1
|
||||
legend([h1(1) h2(1) h3(1)],'Data','FRVF','Deviation');
|
||||
else
|
||||
legend([h1(1) h2(1)],'Data','FRVF');
|
||||
end
|
||||
end
|
||||
if opts.phaseplot==1
|
||||
figure(2),
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase angle [deg]');
|
||||
%title('Approximation of f');
|
||||
if opts.legend==1
|
||||
legend([h4(1) h5(1)],'Data','FRVF');
|
||||
end
|
||||
end
|
||||
drawnow;
|
||||
end
|
||||
fit=fit.';
|
||||
|
||||
|
||||
end %if skip_res~=1
|
||||
|
||||
A=SERA;
|
||||
poles=A;
|
||||
if opts.skip_res~=1
|
||||
B=SERB; C=SERC; D=SERD; E=SERE;
|
||||
else
|
||||
B=ones(N,1); C=zeros(Nc,N); D=zeros(Nc,Nc); E=zeros(Nc,Nc); rmserr=0;
|
||||
end;
|
||||
|
||||
|
||||
%========================================
|
||||
% Convert into real state-space model
|
||||
%========================================
|
||||
if opts.cmplx_ss~=1
|
||||
|
||||
A=diag(sparse(A));
|
||||
|
||||
cindex=zeros(1,N);
|
||||
for m=1:N
|
||||
if imag(A(m,m))~=0
|
||||
if m==1
|
||||
cindex(m)=1;
|
||||
else
|
||||
if cindex(m-1)==0 || cindex(m-1)==2
|
||||
cindex(m)=1; cindex(m+1)=2;
|
||||
else
|
||||
cindex(m)=2;
|
||||
end
|
||||
end
|
||||
end
|
||||
end
|
||||
|
||||
n=0;
|
||||
for m=1:N
|
||||
n=n+1;
|
||||
if cindex(m)==1
|
||||
a=A(n,n); a1=real(a); a2=imag(a);
|
||||
c=C(:,n); c1=real(c); c2=imag(c);
|
||||
b=B(n,:); b1=2*real(b); b2=-2*imag(b);
|
||||
Ablock=[a1 a2;-a2 a1];
|
||||
|
||||
A(n:n+1,n:n+1)=Ablock;
|
||||
C(:,n)=c1;
|
||||
C(:,n+1)=c2;
|
||||
B(n,:)=b1;
|
||||
B(n+1,:)=b2;
|
||||
end
|
||||
end
|
||||
|
||||
else
|
||||
A=sparse(diag(A)); % A is complex, make it diagonal
|
||||
end %if cmplx_ss~=1
|
||||
|
||||
SER.A=A; SER.B=B; SER.C=C; SER.D=D; SER.E=E;
|
||||
|
||||
|
287
matlab/test_apa_1_basic_meas.m
Normal file
287
matlab/test_apa_1_basic_meas.m
Normal file
@ -0,0 +1,287 @@
|
||||
%% Clear Workspace and Close figures
|
||||
clear; close all; clc;
|
||||
|
||||
%% Intialize Laplace variable
|
||||
s = zpk('s');
|
||||
|
||||
%% Path for functions, data and scripts
|
||||
addpath('./src/'); % Path for scripts
|
||||
addpath('./mat/'); % Path for data
|
||||
|
||||
%% Colors for the figures
|
||||
colors = colororder;
|
||||
|
||||
% Geometrical Measurements
|
||||
% <<sec:test_apa_geometrical_measurements>>
|
||||
|
||||
% To measure the flatness of the two mechanical interfaces of the APA300ML, a small measurement bench is installed on top of a metrology granite with very good flatness.
|
||||
|
||||
% As shown in Figure ref:fig:test_apa_flatness_setup, the APA is fixed to a clamp while a measuring probe[fn:3] is used to measure the height of 4 points on each of the APA300ML interfaces.
|
||||
|
||||
% From the X-Y-Z coordinates of the measured 8 points, the flatness is estimated by best fitting[fn:4] a plane through all the points.
|
||||
|
||||
% #+name: fig:test_apa_flatness_setup
|
||||
% #+attr_latex: :width 0.4\linewidth
|
||||
% #+caption: Measurement setup for flatness estimation of the two mechanical interfaces
|
||||
% [[file:figs/test_apa_flatness_setup.png]]
|
||||
|
||||
|
||||
%% Measured height for all the APA at the 8 locations
|
||||
apa1 = 1e-6*[0, -0.5 , 3.5 , 3.5 , 42 , 45.5, 52.5 , 46];
|
||||
apa2 = 1e-6*[0, -2.5 , -3 , 0 , -1.5 , 1 , -2 , -4];
|
||||
apa3 = 1e-6*[0, -1.5 , 15 , 17.5 , 6.5 , 6.5 , 21 , 23];
|
||||
apa4 = 1e-6*[0, 6.5 , 14.5 , 9 , 16 , 22 , 29.5 , 21];
|
||||
apa5 = 1e-6*[0, -12.5, 16.5 , 28.5 , -43 , -52 , -22.5, -13.5];
|
||||
apa6 = 1e-6*[0, -8 , -2 , 5 , -57.5, -62 , -55.5, -52.5];
|
||||
apa7 = 1e-6*[0, 9 , -18.5, -30 , 31 , 46.5, 16.5 , 7.5];
|
||||
|
||||
apa = {apa1, apa2, apa3, apa4, apa5, apa6, apa7};
|
||||
|
||||
%% X-Y positions of the measurements points
|
||||
W = 20e-3; % Width [m]
|
||||
L = 61e-3; % Length [m]
|
||||
d = 1e-3; % Distance from border [m]
|
||||
l = 15.5e-3; % [m]
|
||||
|
||||
pos = [[-L/2 + d, W/2 - d];
|
||||
[-L/2 + l - d, W/2 - d];
|
||||
[-L/2 + l - d, -W/2 + d];
|
||||
[-L/2 + d, -W/2 + d];
|
||||
[L/2 - l + d, W/2 - d];
|
||||
[L/2 - d, W/2 - d];
|
||||
[L/2 - d, -W/2 + d];
|
||||
[L/2 - l + d, -W/2 + d]]';
|
||||
|
||||
%% Using fminsearch to find the best fitting plane
|
||||
apa_d = zeros(1, 7); % Measured flatness of the APA
|
||||
for i = 1:7
|
||||
fun = @(x)max(abs(([pos; apa{i}]-[0;0;x(1)])'*([x(2:3);1]/norm([x(2:3);1]))));
|
||||
x0 = [0;0;0];
|
||||
[x, min_d] = fminsearch(fun,x0);
|
||||
apa_d(i) = min_d;
|
||||
end
|
||||
|
||||
% Stroke Measurement
|
||||
% <<sec:test_apa_stroke_measurements>>
|
||||
|
||||
% The goal is here to verify that the stroke of the APA300ML is as specified in the datasheet.
|
||||
% To do so, one side of the APA is fixed to the granite, and a displacement probe[fn:2] is located on the other side as shown in Figure ref:fig:test_apa_stroke_bench.
|
||||
|
||||
% Then, the voltage across the two actuator stacks is varied from $-20\,V$ to $150\,V$ using a DAC and a voltage amplifier.
|
||||
% Note that the voltage is here slowly varied as the displacement probe has a very low measurement bandwidth (see Figure ref:fig:test_apa_stroke_bench, left).
|
||||
|
||||
% #+name: fig:test_apa_stroke_bench
|
||||
% #+caption: Bench to measured the APA stroke
|
||||
% #+attr_latex: :width 0.9\linewidth
|
||||
% [[file:figs/test_apa_stroke_bench.jpg]]
|
||||
|
||||
% The measured APA displacement is shown as a function of the applied voltage in Figure ref:fig:test_apa_stroke_result, right.
|
||||
|
||||
% Typical hysteresis curves for piezoelectric stack actuators can be observed.
|
||||
% The measured stroke is approximately $250\,\mu m$ when using only two of the three stacks, which is enough for the current application.
|
||||
% This is even above what is specified as the nominal stroke in the data-sheet ($304\,\mu m$, therefore $\approx 200\,\mu m$ if only two stacks are used).
|
||||
|
||||
% It is clear from Figure ref:fig:test_apa_stroke_result that "APA 3" has an issue compared to the other units.
|
||||
% This confirms the abnormal electrical measurements made in Section ref:sec:test_apa_electrical_measurements.
|
||||
% This unit was send sent back to Cedrat and a new one was shipped back.
|
||||
% From now on, only the six APA that behave as expected will be used.
|
||||
|
||||
|
||||
%% Load the measured strokes
|
||||
load('meas_apa_stroke.mat', 'apa300ml_2s')
|
||||
|
||||
%% Results of the measured APA stroke
|
||||
figure;
|
||||
tiledlayout(1, 2, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
% Generated voltage across the two piezoelectric stack actuators to estimate the stroke of the APA300ML
|
||||
ax1 = nexttile();
|
||||
plot(apa300ml_2s{1}.t - apa300ml_2s{1}.t(1), 20*apa300ml_2s{1}.V, 'k-')
|
||||
xlabel('Time [s]'); ylabel('Voltage [V]')
|
||||
ylim([-20, 160])
|
||||
|
||||
% Measured displacement as a function of the applied voltage
|
||||
ax2 = nexttile();
|
||||
hold on;
|
||||
for i = 1:7
|
||||
plot(20*apa300ml_2s{i}.V, 1e6*apa300ml_2s{i}.d, 'DisplayName', sprintf('APA %i', i))
|
||||
end
|
||||
hold off;
|
||||
xlabel('Voltage [V]'); ylabel('Displacement [$\mu m$]')
|
||||
legend('location', 'southwest', 'FontSize', 8)
|
||||
xlim([-20, 150]); ylim([-250, 0]);
|
||||
|
||||
% X-Bending Mode
|
||||
|
||||
% The vibrometer is setup to measure the X-bending motion is shown in Figure ref:fig:test_apa_meas_setup_X_bending.
|
||||
% The APA is excited with an instrumented hammer having a solid metallic tip.
|
||||
% The impact point is on the back-side of the APA aligned with the top measurement point.
|
||||
|
||||
% #+name: fig:test_apa_meas_setup_X_bending
|
||||
% #+caption: X-Bending measurement setup
|
||||
% #+attr_latex: :width 0.7\linewidth
|
||||
% [[file:figs/test_apa_meas_setup_X_bending.jpg]]
|
||||
|
||||
% The data is loaded.
|
||||
|
||||
%% Load Data
|
||||
bending_X = load('apa300ml_bending_X_top.mat');
|
||||
|
||||
|
||||
|
||||
% The configuration (Sampling time and windows) for =tfestimate= is done:
|
||||
|
||||
%% Spectral Analysis setup
|
||||
Ts = bending_X.Track1_X_Resolution; % Sampling Time [s]
|
||||
Nfft = floor(1/Ts);
|
||||
win = hanning(Nfft);
|
||||
Noverlap = floor(Nfft/2);
|
||||
|
||||
|
||||
|
||||
% The transfer function from the input force to the output "rotation" (difference between the two measured distances).
|
||||
|
||||
%% Compute the transfer function from applied force to measured rotation
|
||||
[G_bending_X, f] = tfestimate(bending_X.Track1, bending_X.Track2, win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
|
||||
|
||||
% The result is shown in Figure ref:fig:test_apa_meas_freq_bending_x.
|
||||
|
||||
% The can clearly observe a nice peak at 280Hz, and then peaks at the odd "harmonics" (third "harmonic" at 840Hz, and fifth "harmonic" at 1400Hz).
|
||||
|
||||
%% Plot the transfer function
|
||||
figure;
|
||||
hold on;
|
||||
plot(f, abs(G_bending_X), 'k-');
|
||||
hold off;
|
||||
set(gca, 'Xscale', 'log'); set(gca, 'Yscale', 'log');
|
||||
xlabel('Frequency [Hz]'); ylabel('Amplitude');
|
||||
xlim([50, 2e3]); ylim([1e-5, 2e-1]);
|
||||
text(280, 5.5e-2,{'280Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
text(840, 2.0e-3,{'840Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
text(1400, 7.0e-3,{'1400Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
|
||||
% Y-Bending Mode
|
||||
|
||||
% The setup to measure the Y-bending is shown in Figure ref:fig:test_apa_meas_setup_Y_bending.
|
||||
|
||||
% The impact point of the instrumented hammer is located on the back surface of the top interface (on the back of the 2 measurements points).
|
||||
|
||||
% #+name: fig:test_apa_meas_setup_Y_bending
|
||||
% #+caption: Y-Bending measurement setup
|
||||
% #+attr_latex: :width 0.7\linewidth
|
||||
% [[file:figs/test_apa_meas_setup_Y_bending.jpg]]
|
||||
|
||||
% The data is loaded, and the transfer function from the force to the measured rotation is computed.
|
||||
|
||||
%% Load Data
|
||||
bending_Y = load('apa300ml_bending_Y_top.mat');
|
||||
|
||||
%% Compute the transfer function
|
||||
[G_bending_Y, ~] = tfestimate(bending_Y.Track1, bending_Y.Track2, win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
|
||||
|
||||
% The results are shown in Figure ref:fig:test_apa_meas_freq_bending_y.
|
||||
% The main resonance is at 412Hz, and we also see the third "harmonic" at 1220Hz.
|
||||
|
||||
|
||||
%% Plot the transfer function
|
||||
figure;
|
||||
hold on;
|
||||
plot(f, abs(G_bending_Y), 'k-');
|
||||
hold off;
|
||||
set(gca, 'Xscale', 'log'); set(gca, 'Yscale', 'log');
|
||||
xlabel('Frequency [Hz]'); ylabel('Amplitude');
|
||||
xlim([50, 2e3]); ylim([1e-5, 3e-2])
|
||||
text(412, 1.5e-2,{'412Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
text(1218, 1.5e-2,{'1220Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
|
||||
% Z-Torsion Mode
|
||||
|
||||
% Finally, we measure the Z-torsion resonance as shown in Figure ref:fig:test_apa_meas_setup_torsion_bis.
|
||||
|
||||
% The excitation is shown on the other side of the APA, on the side to excite the torsion motion.
|
||||
|
||||
% #+name: fig:test_apa_meas_setup_torsion_bis
|
||||
% #+caption: Z-Torsion measurement setup
|
||||
% #+attr_latex: :width 0.7\linewidth
|
||||
% [[file:figs/test_apa_meas_setup_torsion_bis.jpg]]
|
||||
|
||||
% The data is loaded, and the transfer function computed.
|
||||
|
||||
%% Load Data
|
||||
torsion = load('apa300ml_torsion_left.mat');
|
||||
|
||||
%% Compute transfer function
|
||||
[G_torsion, ~] = tfestimate(torsion.Track1, torsion.Track2, win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
|
||||
|
||||
% The results are shown in Figure ref:fig:test_apa_meas_freq_torsion_z.
|
||||
% We observe a first peak at 267Hz, which corresponds to the X-bending mode that was measured at 280Hz.
|
||||
% And then a second peak at 415Hz, which corresponds to the X-bending mode that was measured at 412Hz.
|
||||
% A third mode at 800Hz could correspond to this torsion mode.
|
||||
|
||||
|
||||
%% Plot the transfer function
|
||||
figure;
|
||||
hold on;
|
||||
plot(f, abs(G_torsion), 'k-');
|
||||
hold off;
|
||||
set(gca, 'Xscale', 'log'); set(gca, 'Yscale', 'log');
|
||||
xlabel('Frequency [Hz]'); ylabel('Amplitude');
|
||||
xlim([50, 2e3]); ylim([1e-5, 2e-2])
|
||||
text(415, 4.3e-3,{'415Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
text(267, 8e-4,{'267Hz'}, 'VerticalAlignment', 'bottom','HorizontalAlignment','center')
|
||||
text(800, 6e-4,{'800Hz'}, 'VerticalAlignment', 'bottom','HorizontalAlignment','center')
|
||||
|
||||
|
||||
|
||||
% #+name: fig:test_apa_meas_freq_torsion_z
|
||||
% #+caption: Obtained FRF for the Z-torsion
|
||||
% #+RESULTS:
|
||||
% [[file:figs/test_apa_meas_freq_torsion_z.png]]
|
||||
|
||||
% In order to verify that, the APA is excited on the top part such that the torsion mode should not be excited.
|
||||
|
||||
%% Load data
|
||||
torsion = load('apa300ml_torsion_top.mat');
|
||||
|
||||
%% Compute transfer function
|
||||
[G_torsion_top, ~] = tfestimate(torsion.Track1, torsion.Track2, win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
|
||||
|
||||
% The two FRF are compared in Figure ref:fig:test_apa_meas_freq_torsion_z_comp.
|
||||
% It is clear that the first two modes does not correspond to the torsional mode.
|
||||
% Maybe the resonance at 800Hz, or even higher resonances. It is difficult to conclude here.
|
||||
|
||||
%% Plot the two transfer functions
|
||||
figure;
|
||||
hold on;
|
||||
plot(f, abs(G_torsion), 'k-', 'DisplayName', 'Left excitation');
|
||||
plot(f, abs(G_torsion_top), '-', 'DisplayName', 'Top excitation');
|
||||
hold off;
|
||||
set(gca, 'Xscale', 'log'); set(gca, 'Yscale', 'log');
|
||||
xlabel('Frequency [Hz]'); ylabel('Amplitude');
|
||||
xlim([50, 2e3]); ylim([1e-5, 2e-2])
|
||||
text(415, 4.3e-3,{'415Hz'},'VerticalAlignment','bottom','HorizontalAlignment','center')
|
||||
text(267, 8e-4,{'267Hz'}, 'VerticalAlignment', 'bottom','HorizontalAlignment','center')
|
||||
text(800, 2e-3,{'800Hz'}, 'VerticalAlignment', 'bottom','HorizontalAlignment','center')
|
||||
legend('location', 'northwest');
|
||||
|
||||
% Compare
|
||||
% The three measurements are shown in Figure ref:fig:test_apa_meas_freq_compare.
|
||||
|
||||
figure;
|
||||
hold on;
|
||||
plot(f, abs(G_torsion), 'DisplayName', 'Torsion');
|
||||
plot(f, abs(G_bending_X), 'DisplayName', 'Bending - X');
|
||||
plot(f, abs(G_bending_Y), 'DisplayName', 'Bending - Y');
|
||||
hold off;
|
||||
set(gca, 'Xscale', 'log'); set(gca, 'Yscale', 'log');
|
||||
xlabel('Frequency [Hz]'); ylabel('Amplitude');
|
||||
xlim([50, 2e3]); ylim([1e-5, 1e-1]);
|
||||
legend('location', 'southeast');
|
575
matlab/test_apa_2_dynamics.m
Normal file
575
matlab/test_apa_2_dynamics.m
Normal file
@ -0,0 +1,575 @@
|
||||
%% Clear Workspace and Close figures
|
||||
clear; close all; clc;
|
||||
|
||||
%% Intialize Laplace variable
|
||||
s = zpk('s');
|
||||
|
||||
%% Path for functions, data and scripts
|
||||
addpath('./src/'); % Path for scripts
|
||||
addpath('./mat/'); % Path for data
|
||||
|
||||
%% Colors for the figures
|
||||
colors = colororder;
|
||||
|
||||
% Hysteresis
|
||||
% <<ssec:test_apa_hysteresis>>
|
||||
|
||||
% As the payload is vertically guided without friction, the hysteresis of the APA can be estimated from the motion of the payload.
|
||||
|
||||
% A quasi static sinusoidal excitation $V_a$ with an offset of $65\,V$ (halfway between $-20\,V$ and $150\,V$), and an amplitude varying from $4\,V$ up to $80\,V$.
|
||||
|
||||
% For each excitation amplitude, the vertical displacement $d_e$ of the mass is measured and displayed as a function of the applied voltage..
|
||||
|
||||
|
||||
%% Load measured data - hysteresis
|
||||
apa_hyst = load('frf_data_1_hysteresis.mat', 't', 'u', 'de');
|
||||
|
||||
% Initial time set to zero
|
||||
apa_hyst.t = apa_hyst.t - apa_hyst.t(1);
|
||||
|
||||
ampls = [0.1, 0.2, 0.4, 1, 2, 4]; % Excitation voltage amplitudes
|
||||
|
||||
|
||||
|
||||
% The measured displacements as a function of the output voltages are shown in Figure ref:fig:test_apa_meas_hysteresis.
|
||||
% It is interesting to see that the hysteresis is increasing with the excitation amplitude.
|
||||
|
||||
|
||||
%% Measured displacement as a function of the output voltage
|
||||
figure;
|
||||
|
||||
hold on;
|
||||
for i = [6,5,4,2]
|
||||
i_lim = apa_hyst.t > i*5-1 & apa_hyst.t < i*5;
|
||||
plot(20*apa_hyst.u(i_lim), 1e6*detrend(apa_hyst.de(i_lim), 0), ...
|
||||
'DisplayName', sprintf('$V_a = 65 + %.0f \\sin (\\omega t) \\ [V]$', 20*ampls(i)))
|
||||
end
|
||||
hold off;
|
||||
xlabel('Stack Voltage $V_a$ [V]'); ylabel('Displacement $d_e$ [$\mu$m]');
|
||||
legend('location', 'northeast', 'FontSize', 8, 'NumColumns', 1);
|
||||
xlim([-20, 150]);
|
||||
ylim([-120, 120]);
|
||||
|
||||
% Axial stiffness
|
||||
% <<ssec:test_apa_stiffness>>
|
||||
|
||||
% In order to estimate the stiffness of the APA, a weight with known mass $m_a = 6.4\,\text{kg}$ is added on top of the suspended granite and the deflection $d_e$ is measured using the encoder.
|
||||
|
||||
% The APA stiffness can then be estimated from equation eqref:eq:test_apa_stiffness.
|
||||
|
||||
% \begin{equation} \label{eq:test_apa_stiffness}
|
||||
% k_{\text{apa}} = \frac{m_a g}{\Delta d_e}
|
||||
% \end{equation}
|
||||
|
||||
|
||||
%% Load data for stiffness measurement
|
||||
apa_nums = [1 2 4 5 6 8];
|
||||
apa_mass = {};
|
||||
for i = 1:length(apa_nums)
|
||||
apa_mass(i) = {load(sprintf('frf_data_%i_add_mass_closed_circuit.mat', apa_nums(i)), 't', 'de')};
|
||||
% The initial displacement is set to zero
|
||||
apa_mass{i}.de = apa_mass{i}.de - mean(apa_mass{i}.de(apa_mass{i}.t<11));
|
||||
end
|
||||
|
||||
added_mass = 6.4; % Added mass [kg]
|
||||
|
||||
|
||||
|
||||
% The measured displacement $d_e$ as a function of time is shown in Figure ref:fig:test_apa_meas_stiffness_time.
|
||||
% It can be seen that there are some drifts in the measured displacement (probably due to piezoelectric creep) and the that displacement does not come back to the initial position after the mass is removed (probably due to piezoelectric hysteresis).
|
||||
% These two effects induce some uncertainties in the measured stiffness.
|
||||
|
||||
|
||||
%% Plot the deflection at a function of time
|
||||
figure;
|
||||
hold on;
|
||||
plot(apa_mass{2}.t(1:100:end)-apa_mass{2}.t(1), 1e6*apa_mass{2}.de(1:100:end), 'k-');
|
||||
plot([0,20], [-0.4, -0.4], 'k--', 'LineWidth', 0.5)
|
||||
plot([0,20], [-4.5, -4.5], 'k--', 'LineWidth', 0.5)
|
||||
plot([0,20], [-37.4, -37.4], 'k--', 'LineWidth', 0.5)
|
||||
% first stroke for stiffness measurements
|
||||
anArrow = annotation('doublearrow', 'LineWidth', 0.5);
|
||||
anArrow.Parent = gca;
|
||||
anArrow.Position = [2, -0.4, 0, -37];
|
||||
text(2.5, -20, sprintf('$d_1$'), 'horizontalalignment', 'left');
|
||||
|
||||
% second stroke for stiffness measurements
|
||||
anArrow = annotation('doublearrow', 'LineWidth', 0.5);
|
||||
anArrow.Parent = gca;
|
||||
anArrow.Position = [18, -37.4, 0, 32.9];
|
||||
text(18.5, -20, sprintf('$d_2$'), 'horizontalalignment', 'left');
|
||||
|
||||
% annotation('textarrow',[],y,'String',' Growth ','FontSize',13,'Linewidth',2)
|
||||
hold off;
|
||||
xlabel('Time [s]'); ylabel('Displacement $d_e$ [$\mu$m]');
|
||||
|
||||
|
||||
|
||||
% #+name: tab:test_apa_measured_stiffnesses
|
||||
% #+caption: Measured stiffnesses (in $N/\mu m$)
|
||||
% #+attr_latex: :environment tabularx :width 0.2\linewidth :align ccc
|
||||
% #+attr_latex: :center t :booktabs t :float t
|
||||
% #+RESULTS:
|
||||
% | APA | $k_1$ | $k_2$ |
|
||||
% |-----+-------+-------|
|
||||
% | 1 | 1.68 | 1.9 |
|
||||
% | 2 | 1.69 | 1.9 |
|
||||
% | 4 | 1.7 | 1.91 |
|
||||
% | 5 | 1.7 | 1.93 |
|
||||
% | 6 | 1.7 | 1.92 |
|
||||
% | 8 | 1.73 | 1.98 |
|
||||
|
||||
% The stiffness can also be computed using equation eqref:eq:test_apa_res_freq by knowing the main vertical resonance frequency $\omega_z \approx 94\,\text{Hz}$ (estimated by the dynamical measurements shown in section ref:ssec:test_apa_meas_frf_disp) and the suspended mass $m_{\text{sus}} = 5.7\,\text{kg}$.
|
||||
|
||||
% \begin{equation} \label{eq:test_apa_res_freq}
|
||||
% \omega_z = \sqrt{\frac{k}{m_{\text{sus}}}}
|
||||
% \end{equation}
|
||||
|
||||
% The obtain stiffness is $k \approx 2\,N/\mu m$ which is close to the values found in the documentation and by the "static deflection" method.
|
||||
|
||||
|
||||
% However, changes in the electrical impedance connected to the piezoelectric stacks impacts the mechanical compliance (or stiffness) of the piezoelectric stack [[cite:&reza06_piezoel_trans_vibrat_contr_dampin chap. 2]].
|
||||
|
||||
% To estimate this effect, the stiffness of the APA if measured using the "static deflection" method in two cases:
|
||||
% - $k_{\text{os}}$: piezoelectric stacks left unconnected (or connect to the high impedance ADC)
|
||||
% - $k_{\text{sc}}$: piezoelectric stacks short circuited (or connected to the voltage amplifier with small output impedance)
|
||||
|
||||
% The open-circuit stiffness is estimated at $k_{\text{oc}} \approx 2.3\,N/\mu m$ and the closed-circuit stiffness $k_{\text{sc}} \approx 1.7\,N/\mu m$.
|
||||
|
||||
|
||||
%% Load Data
|
||||
add_mass_oc = load('frf_data_1_add_mass_open_circuit.mat', 't', 'de');
|
||||
add_mass_cc = load('frf_data_1_add_mass_closed_circuit.mat', 't', 'de');
|
||||
|
||||
%% Zero displacement at initial time
|
||||
add_mass_oc.de = add_mass_oc.de - mean(add_mass_oc.de(add_mass_oc.t<11));
|
||||
add_mass_cc.de = add_mass_cc.de - mean(add_mass_cc.de(add_mass_cc.t<11));
|
||||
|
||||
%% Estimation of the stiffness in Open Circuit and Closed-Circuit
|
||||
apa_k_oc = 9.8 * added_mass / (mean(add_mass_oc.de(add_mass_oc.t > 12 & add_mass_oc.t < 12.5)) - mean(add_mass_oc.de(add_mass_oc.t > 20 & add_mass_oc.t < 20.5)));
|
||||
apa_k_sc = 9.8 * added_mass / (mean(add_mass_cc.de(add_mass_cc.t > 12 & add_mass_cc.t < 12.5)) - mean(add_mass_cc.de(add_mass_cc.t > 20 & add_mass_cc.t < 20.5)));
|
||||
|
||||
%% Estimated coupling factor
|
||||
sqrt(1 - apa_k_sc/apa_k_oc)
|
||||
|
||||
% Dynamics
|
||||
% <<ssec:test_apa_meas_dynamics>>
|
||||
|
||||
% In this section, the dynamics of the system from the excitation voltage $u$ to encoder measured displacement $d_e$ and to the force sensor voltage $V_s$ is identified.
|
||||
|
||||
|
||||
%% Identification using sweep sine (low frequency)
|
||||
load('frf_data_sweep.mat');
|
||||
load('frf_data_noise_hf.mat');
|
||||
|
||||
%% Sampling Frequency
|
||||
Ts = 1e-4; % Sampling Time [s]
|
||||
Fs = 1/Ts; % Sampling Frequency [Hz]
|
||||
|
||||
%% "Hanning" windows used for the spectral analysis:
|
||||
Nfft = floor(2/Ts);
|
||||
win = hanning(Nfft);
|
||||
Noverlap = floor(Nfft/2);
|
||||
|
||||
%% Separation of frequencies: low freqs using sweep sine, and high freq using noise
|
||||
% Only used to have the frequency vector "f"
|
||||
[~, f] = tfestimate(apa_sweep{1}.u, apa_sweep{1}.de, win, Noverlap, Nfft, 1/Ts);
|
||||
i_lf = f <= 350;
|
||||
i_hf = f > 350;
|
||||
|
||||
%% FRF estimation of the transfer function from u to de
|
||||
enc_frf = zeros(length(f), length(apa_nums));
|
||||
for i = 1:length(apa_nums)
|
||||
[frf_lf, ~] = tfestimate(apa_sweep{i}.u, apa_sweep{i}.de, win, Noverlap, Nfft, 1/Ts);
|
||||
[frf_hf, ~] = tfestimate(apa_noise_hf{i}.u, apa_noise_hf{i}.de, win, Noverlap, Nfft, 1/Ts);
|
||||
enc_frf(:, i) = [frf_lf(i_lf); frf_hf(i_hf)];
|
||||
end
|
||||
|
||||
%% FRF estimation of the transfer function from u to Vs
|
||||
iff_frf = zeros(length(f), length(apa_nums));
|
||||
for i = 1:length(apa_nums)
|
||||
[frf_lf, ~] = tfestimate(apa_sweep{i}.u, apa_sweep{i}.Vs, win, Noverlap, Nfft, 1/Ts);
|
||||
[frf_hf, ~] = tfestimate(apa_noise_hf{i}.u, apa_noise_hf{i}.Vs, win, Noverlap, Nfft, 1/Ts);
|
||||
iff_frf(:, i) = [frf_lf(i_lf); frf_hf(i_hf)];
|
||||
end
|
||||
|
||||
%% Save the identified dynamics for further analysis
|
||||
save('mat/meas_apa_frf.mat', 'f', 'Ts', 'enc_frf', 'iff_frf', 'apa_nums');
|
||||
|
||||
|
||||
|
||||
% The obtained transfer functions for the 6 APA between the excitation voltage $u$ and the encoder displacement $d_e$ are shown in Figure ref:fig:test_apa_frf_encoder.
|
||||
% The obtained transfer functions are close to a mass-spring-damper system.
|
||||
% The following can be observed:
|
||||
% - A "stiffness line" indicating a static gain equal to $\approx -17\,\mu m/V$.
|
||||
% The minus sign comes from the fact that an increase in voltage stretches the piezoelectric stack that then reduces the height of the APA
|
||||
% - A lightly damped resonance at $95\,\text{Hz}$
|
||||
% - A "mass line" up to $\approx 800\,\text{Hz}$, above which some resonances appear
|
||||
|
||||
|
||||
%% Plot the FRF from u to de
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(enc_frf(:, i)), ...
|
||||
'DisplayName', sprintf('APA %i', apa_nums(i)));
|
||||
end
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $d_e/u$ [m/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
legend('location', 'northeast', 'FontSize', 8, 'NumColumns', 2);
|
||||
ylim([1e-8, 1e-3]);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(enc_frf(:, i)));
|
||||
end
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:test_apa_frf_encoder
|
||||
% #+caption: Estimated Frequency Response Function from generated voltage $u$ to the encoder displacement $d_e$ for the 6 APA300ML
|
||||
% #+RESULTS:
|
||||
% [[file:figs/test_apa_frf_encoder.png]]
|
||||
|
||||
% The dynamics from $u$ to the measured voltage across the sensor stack $V_s$ is also identified and shown in Figure ref:fig:test_apa_frf_force.
|
||||
|
||||
% A lightly damped resonance is observed at $95\,\text{Hz}$ and a lightly damped anti-resonance at $41\,\text{Hz}$.
|
||||
% No additional resonances is present up to at least $2\,\text{kHz}$ indicating at Integral Force Feedback can be applied without stability issues from high frequency flexible modes.
|
||||
|
||||
% As illustrated by the Root Locus, the poles of the closed-loop system converges to the zeros of the open-loop plant.
|
||||
% Suppose that a controller with a very high gain is implemented such that the voltage $V_s$ across the sensor stack is zero.
|
||||
% In that case, because of the very high controller gain, no stress and strain is present on the sensor stack (and on the actuator stacks are well, as they are both in series).
|
||||
% Such closed-loop system would therefore virtually corresponds to a system for which the piezoelectric stacks have been removed and just the mechanical shell is kept.
|
||||
% From this analysis, the axial stiffness of the shell can be estimated to be $k_{\text{shell}} = 5.7 \cdot (2\pi \cdot 41)^2 = 0.38\,N/\mu m$.
|
||||
% # TODO - Compare with FEM result
|
||||
|
||||
% Such reasoning can lead to very interesting insight into the system just from an open-loop identification.
|
||||
|
||||
|
||||
%% Plot the FRF from u to Vs
|
||||
figure;
|
||||
tiledlayout(2, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(iff_frf(:, i)), ...
|
||||
'DisplayName', sprintf('APA %i', apa_nums(i)));
|
||||
end
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $V_s/u$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-2, 1e2]);
|
||||
legend('location', 'southeast', 'FontSize', 8, 'NumColumns', 2);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(iff_frf(:, i)));
|
||||
end
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
% Effect of the resistor on the IFF Plant
|
||||
% <<ssec:test_apa_resistance_sensor_stack>>
|
||||
|
||||
% A resistor $R \approx 80.6\,k\Omega$ is added in parallel with the sensor stack which has the effect to form a high pass filter with the capacitance of the stack.
|
||||
|
||||
% As explain before, this is done for two reasons:
|
||||
% 1. Limit the voltage offset due to the input bias current of the ADC
|
||||
% 2. Limit the low frequency gain
|
||||
|
||||
% The (low frequency) transfer function from $u$ to $V_s$ with and without this resistor have been measured and are compared in Figure ref:fig:test_apa_effect_resistance.
|
||||
% It is confirmed that the added resistor as the effect of adding an high pass filter with a cut-off frequency of $\approx 0.35\,\text{Hz}$.
|
||||
|
||||
|
||||
%% Load the data
|
||||
wi_k = load('frf_data_1_sweep_lf_with_R.mat', 't', 'Vs', 'Va'); % With the resistor
|
||||
wo_k = load('frf_data_1_sweep_lf.mat', 't', 'Vs', 'Va'); % Without the resistor
|
||||
|
||||
%% Large Hanning window for good low frequency estimate
|
||||
Nfft = floor(50/Ts);
|
||||
win = hanning(Nfft);
|
||||
Noverlap = floor(Nfft/2);
|
||||
|
||||
%% Compute the transfer functions from Va to Vs
|
||||
[frf_wo_k, f] = tfestimate(wo_k.Va, wo_k.Vs, win, Noverlap, Nfft, 1/Ts);
|
||||
[frf_wi_k, ~] = tfestimate(wi_k.Va, wi_k.Vs, win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
%% Model for the high pass filter
|
||||
C = 5.1e-6; % Sensor Stack capacitance [F]
|
||||
R = 80.6e3; % Parallel Resistor [Ohm]
|
||||
|
||||
f0 = 1/(2*pi*R*C); % Crossover frequency of RC HPF [Hz]
|
||||
|
||||
G_hpf = 0.6*(s/2*pi*f0)/(1 + s/2*pi*f0);
|
||||
|
||||
%% Compare the HPF model and the measured FRF
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
plot(f, abs(frf_wo_k), 'DisplayName', 'Without $R$');
|
||||
plot(f, abs(frf_wi_k), 'DisplayName', 'With $R$');
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $V_s/u$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-1, 1e0]);
|
||||
legend('location', 'southeast')
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
plot(f, 180/pi*angle(frf_wo_k));
|
||||
plot(f, 180/pi*angle(frf_wi_k));
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:45:360); ylim([-45, 90]);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([0.2, 8]);
|
||||
|
||||
% Integral Force Feedback
|
||||
% <<ssec:test_apa_iff_locus>>
|
||||
|
||||
% This test bench can also be used to estimate the damping added by the implementation of an Integral Force Feedback strategy.
|
||||
|
||||
|
||||
%% Load identification Data
|
||||
data = load("2023-03-17_11-28_iff_plant.mat");
|
||||
|
||||
%% Spectral Analysis setup
|
||||
Ts = 1e-4; % Sampling Time [s]
|
||||
Nfft = floor(5/Ts);
|
||||
win = hanning(Nfft);
|
||||
Noverlap = floor(Nfft/2);
|
||||
|
||||
%% Compute the transfer function from applied force to measured rotation
|
||||
[G_iff, f] = tfestimate(data.id_plant, data.Vs, win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
|
||||
|
||||
% First, the transfer function eqref:eq:test_apa_iff_manual_fit is manually tuned to match the identified dynamics from generated voltage $u$ to the measured sensor stack voltage $V_s$ in Section ref:ssec:test_apa_meas_dynamics.
|
||||
|
||||
% The obtained parameter values are $\omega_{\textsc{hpf}} = 0.4\, \text{Hz}$, $\omega_{z} = 42.7\, \text{Hz}$, $\xi_{z} = 0.4\,\%$, $\omega_{p} = 95.2\, \text{Hz}$, $\xi_{p} = 2\,\%$ and $g_0 = 0.64$.
|
||||
|
||||
% \begin{equation} \label{eq:test_apa_iff_manual_fit}
|
||||
% G_{\textsc{iff},m}(s) = g_0 \cdot \frac{1 + 2 \xi_z \frac{s}{\omega_z} + \frac{s^2}{\omega_z^2}}{1 + 2 \xi_p \frac{s}{\omega_p} + \frac{s^2}{\omega_p^2}} \cdot \frac{s}{\omega_{\textsc{hpf}} + s}
|
||||
% \end{equation}
|
||||
|
||||
% The comparison between the identified plant and the manually tuned transfer function is done in Figure ref:fig:test_apa_iff_plant_comp_manual_fit.
|
||||
|
||||
|
||||
%% Basic manually tuned model
|
||||
w0z = 2*pi*42.7; % Zero frequency
|
||||
xiz = 0.004; % Zero damping
|
||||
|
||||
w0p = 2*pi*95.2; % Pole frequency
|
||||
xip = 0.02; % Pole damping
|
||||
|
||||
G_iff_model = exp(-2*s*Ts)*0.64*(1 + 2*xiz/w0z*s + s^2/w0z^2)/(1 + 2*xip/w0p*s + s^2/w0p^2)*(s/(s+2*pi*0.4));
|
||||
|
||||
%% Identified IFF plant and manually tuned model of the plant
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
plot(f, abs(G_iff), 'color', colors(2,:), 'DisplayName', 'Identified plant')
|
||||
plot(f, abs(squeeze(freqresp(G_iff_model, f, 'Hz'))), 'k--', 'DisplayName', 'Manual fit')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $V_s/u$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
legend('location', 'southeast', 'FontSize', 8, 'NumColumns', 1);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
plot(f, 180/pi*angle(G_iff), 'color', colors(2,:));
|
||||
plot(f, 180/pi*angle(squeeze(freqresp(G_iff_model, f, 'Hz'))), 'k--')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:45:360);
|
||||
ylim([-90, 180])
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([0.2, 1e3]);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:test_apa_iff_plant_comp_manual_fit
|
||||
% #+caption: Identified IFF plant and manually tuned model of the plant (a time delay of $200\,\mu s$ is added to the model of the plant to better match the identified phase)
|
||||
% #+RESULTS:
|
||||
% [[file:figs/test_apa_iff_plant_comp_manual_fit.png]]
|
||||
|
||||
% The implemented Integral Force Feedback Controller transfer function is shown in equation eqref:eq:test_apa_Kiff_formula.
|
||||
% It contains an high pass filter (cut-off frequency of $2\,\text{Hz}$) to limit the low frequency gain, a low pass filter to add integral action above $20\,\text{Hz}$, a second low pass filter to add robustness to high frequency resonances and a tunable gain $g$.
|
||||
|
||||
% \begin{equation} \label{eq:test_apa_Kiff_formula}
|
||||
% K_{\textsc{iff}}(s) = -10 \cdot g \cdot \frac{s}{s + 2\pi \cdot 2} \cdot \frac{1}{1 + 2\pi \cdot 20} \cdot \frac{1}{s + 2\pi\cdot 2000}
|
||||
% \end{equation}
|
||||
|
||||
|
||||
%% Integral Force Feedback Controller
|
||||
K_iff = -10*(1/(s + 2*pi*20)) * ... % LPF: provides integral action above 20Hz
|
||||
(s/(s + 2*pi*2)) * ... % HPF: limit low frequency gain
|
||||
(1/(1 + s/2/pi/2e3)); % LPF: more robust to high frequency resonances
|
||||
|
||||
|
||||
|
||||
% To estimate how the dynamics of the APA changes when the Integral Force Feedback controller is implemented, the test bench shown in Figure ref:fig:test_apa_iff_schematic is used.
|
||||
% The transfer function from the "damped" plant input $u\prime$ to the encoder displacement $d_e$ is identified for several IFF controller gains $g$.
|
||||
|
||||
% #+name: fig:test_apa_iff_schematic
|
||||
% #+caption: Figure caption
|
||||
% [[file:figs/test_apa_iff_schematic.png]]
|
||||
|
||||
|
||||
%% Load Data
|
||||
data = load("2023-03-17_14-10_damped_plants_new.mat");
|
||||
|
||||
%% Spectral Analysis setup
|
||||
Ts = 1e-4; % Sampling Time [s]
|
||||
Nfft = floor(1/Ts);
|
||||
win = hanning(Nfft);
|
||||
Noverlap = floor(Nfft/2);
|
||||
|
||||
%% Get the frequency vector
|
||||
[~, f] = tfestimate(data.data(1).id_plant(1:end), data.data(1).dL(1:end), win, Noverlap, Nfft, 1/Ts);
|
||||
|
||||
%% Gains used for analysis are between 1 and 50
|
||||
i_kept = [5:10]
|
||||
|
||||
%% Identify the damped plant from u' to de for different IFF gains
|
||||
G_dL_frf = {zeros(1,length(i_kept))};
|
||||
|
||||
for i = 1:length(i_kept)
|
||||
[G_dL, ~] = tfestimate(data.data(i_kept(i)).id_plant(1:end), data.data(i_kept(i)).dL(1:end), win, Noverlap, Nfft, 1/Ts);
|
||||
G_dL_frf(i) = {G_dL};
|
||||
end
|
||||
|
||||
|
||||
|
||||
% The identified dynamics are then fitted by second order transfer functions.
|
||||
% The comparison between the identified damped dynamics and the fitted second order transfer functions is done in Figure ref:fig:test_apa_identified_damped_plants for different gains $g$.
|
||||
% It is clear that large amount of damping is added when the gain is increased and that the frequency of the pole is shifted to lower frequencies.
|
||||
|
||||
|
||||
%% Fit the data with 2nd order transfer function using vectfit3
|
||||
opts = struct();
|
||||
|
||||
opts.stable = 1; % Enforce stable poles
|
||||
opts.asymp = 1; % Force D matrix to be null
|
||||
opts.relax = 1; % Use vector fitting with relaxed non-triviality constraint
|
||||
opts.skip_pole = 0; % Do NOT skip pole identification
|
||||
opts.skip_res = 0; % Do NOT skip identification of residues (C,D,E)
|
||||
opts.cmplx_ss = 0; % Create real state space model with block diagonal A
|
||||
|
||||
opts.spy1 = 0; % No plotting for first stage of vector fitting
|
||||
opts.spy2 = 0; % Create magnitude plot for fitting of f(s)
|
||||
|
||||
|
||||
Niter = 100; % Number of iteration.
|
||||
N = 2; % Order of approximation
|
||||
poles = [-25 - 1i*60, -25 + 1i*60]; % First get for the pole location
|
||||
|
||||
G_dL_id = {zeros(1,length(i_kept))};
|
||||
|
||||
% Identification just between two frequencies
|
||||
f_keep = (f>20 & f<200);
|
||||
|
||||
for i = 1:length(i_kept)
|
||||
%% Estimate resonance frequency and damping
|
||||
for iter = 1:Niter
|
||||
[G_est, poles, ~, frf_est] = vectfit3(G_dL_frf{i}(f_keep).', 1i*2*pi*f(f_keep)', poles, ones(size(f(f_keep)))', opts);
|
||||
end
|
||||
G_dL_id(i) = {ss(G_est.A, G_est.B, G_est.C, G_est.D)};
|
||||
end
|
||||
|
||||
%% Identified dynamics from u' to de for different IFF gains
|
||||
figure;
|
||||
tiledlayout(1, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile();
|
||||
hold on;
|
||||
for i = 1:length(i_kept)
|
||||
plot(f, abs(G_dL_frf{i}), 'color', [colors(i,:), 1], 'DisplayName', sprintf('g = %.0f', data.gains(i_kept(i))))
|
||||
plot(f, abs(squeeze(freqresp(G_dL_id{i}, f, 'Hz'))), '--', 'color', [colors(i,:), 1], 'HandleVisibility', 'off')
|
||||
end
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
xlabel('Frequency [Hz]'); ylabel('Amplitude $d_L/V_a$ [m/V]');
|
||||
xlim([10, 1e3]);
|
||||
legend('location', 'northeast', 'FontSize', 8, 'NumColumns', 1);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:test_apa_identified_damped_plants
|
||||
% #+caption: Identified dynamics (solid lines) and fitted transfer functions (dashed lines) from $u\prime$ to $d_e$ for different IFF gains
|
||||
% #+RESULTS:
|
||||
% [[file:figs/test_apa_identified_damped_plants.png]]
|
||||
|
||||
% The evolution of the pole in the complex plane as a function of the controller gain $g$ (i.e. the "root locus") is computed:
|
||||
% - using the IFF plant model eqref:eq:test_apa_iff_manual_fit and the implemented controller eqref:eq:test_apa_Kiff_formula
|
||||
% - from the fitted transfer functions of the damped plants experimentally identified for several controller gains
|
||||
|
||||
% The two obtained root loci are compared in Figure ref:fig:test_apa_iff_root_locus and are in good agreement considering that the damped plants were only fitted using a second order transfer function.
|
||||
|
||||
|
||||
%% Root Locus of the APA300ML with Integral Force Feedback
|
||||
% Comparison between the computed root locus from the plant model and the root locus estimated from the damped plant pole identification
|
||||
figure;
|
||||
gains = logspace(-1, 3, 1000);
|
||||
|
||||
figure;
|
||||
hold on;
|
||||
G_iff_poles = pole(G_iff_model);
|
||||
i = imag(G_iff_poles) > 100; % Only keep relevant poles
|
||||
plot(real(G_iff_poles(i)), imag(G_iff_poles(i)), 'kx', ...
|
||||
'DisplayName', '$g = 0$');
|
||||
G_iff_zeros = tzero(G_iff_model);
|
||||
i = imag(G_iff_zeros) > 100; % Only keep relevant zeros
|
||||
plot(real(G_iff_zeros(i)), imag(G_iff_zeros(i)), 'ko', ...
|
||||
'HandleVisibility', 'off');
|
||||
|
||||
for g = gains
|
||||
clpoles = pole(feedback(G_iff_model, g*K_iff, 1));
|
||||
i = imag(clpoles) > 100; % Only keep relevant poles
|
||||
plot(real(clpoles(i)), imag(clpoles(i)), 'k.', ...
|
||||
'HandleVisibility', 'off');
|
||||
end
|
||||
|
||||
for i = 1:length(i_kept)
|
||||
plot(real(pole(G_dL_id{i})), imag(pole(G_dL_id{i})), 'x', 'color', [colors(i,:), 1], 'DisplayName', sprintf('g = %1.f', data.gains(i_kept(i))));
|
||||
end
|
||||
ylim([0, 700]);
|
||||
xlim([-600,100]);
|
||||
xlabel('Real Part')
|
||||
ylabel('Imaginary Part')
|
||||
axis square
|
||||
legend('location', 'northwest');
|
566
matlab/test_apa_3_simscape.m
Normal file
566
matlab/test_apa_3_simscape.m
Normal file
@ -0,0 +1,566 @@
|
||||
%% Clear Workspace and Close figures
|
||||
clear; close all; clc;
|
||||
|
||||
%% Intialize Laplace variable
|
||||
s = zpk('s');
|
||||
|
||||
%% Path for functions, data and scripts
|
||||
addpath('./src/'); % Path for scripts
|
||||
addpath('./mat/'); % Path for data
|
||||
|
||||
addpath('./STEPS/'); % Path for Simscape Model
|
||||
|
||||
%% Open Simscape Model
|
||||
mdl = 'test_apa_simscape'; % Name of the Simulink File
|
||||
open(mdl); % Open Simscape Model
|
||||
|
||||
%% Colors for the figures
|
||||
colors = colororder;
|
||||
|
||||
% First Identification
|
||||
% <<sec:simscape_bench_apa_first_id>>
|
||||
|
||||
% The APA is first initialized with default parameters:
|
||||
|
||||
%% Initialize the structure with default values
|
||||
n_hexapod = struct();
|
||||
n_hexapod.actuator = initializeAPA(...
|
||||
'type', '2dof', ...
|
||||
'Ga', 1, ... % Actuator constant [N/V]
|
||||
'Gs', 1); % Sensor constant [V/m]
|
||||
|
||||
|
||||
|
||||
% The transfer function from excitation voltage $V_a$ (before the amplification of $20$ due to the PD200 amplifier) to:
|
||||
% 1. the sensor stack voltage $V_s$
|
||||
% 2. the measured displacement by the encoder $d_e$
|
||||
|
||||
|
||||
%% Input/Output definition
|
||||
clear io; io_i = 1;
|
||||
io(io_i) = linio([mdl, '/Va'], 1, 'openinput'); io_i = io_i + 1; % DAC Voltage
|
||||
io(io_i) = linio([mdl, '/Vs'], 1, 'openoutput'); io_i = io_i + 1; % Sensor Voltage
|
||||
io(io_i) = linio([mdl, '/de'], 1, 'openoutput'); io_i = io_i + 1; % Encoder
|
||||
|
||||
%% Linearization options
|
||||
opts = linearizeOptions;
|
||||
opts.SampleTime = 0;
|
||||
|
||||
%% Run the linearization
|
||||
Ga = linearize(mdl, io, 0.0, opts);
|
||||
Ga.InputName = {'Va'};
|
||||
Ga.OutputName = {'Vs', 'de', 'da'};
|
||||
|
||||
|
||||
|
||||
% The obtain dynamics are shown in Figure ref:fig:apa_model_bench_bode_vs and ref:fig:apa_model_bench_bode_dl_z.
|
||||
% It can be seen that:
|
||||
% - the shape of these bode plots are very similar to the one measured in Section ref:sec:dynamical_meas_apa expect from a change in gain and exact location of poles and zeros
|
||||
% - there is a sign error for the transfer function from $V_a$ to $V_s$.
|
||||
% This will be corrected by taking a negative "sensor gain".
|
||||
% - the low frequency zero of the transfer function from $V_a$ to $V_s$ is minimum phase as expected.
|
||||
% The measured FRF are showing non-minimum phase zero, but it is most likely due to measurements artifacts.
|
||||
|
||||
|
||||
%% Bode plot of the transfer function from u to taum
|
||||
freqs = logspace(1, 3, 1000);
|
||||
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
plot(freqs, abs(squeeze(freqresp(Ga('Vs', 'Va'), freqs, 'Hz'))), 'k-')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $V_s/V_a$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Ga('Vs', 'Va'), freqs, 'Hz'))), 'k-')
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:45:360);
|
||||
ylim([-180, 0])
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([freqs(1), freqs(end)]);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:apa_model_bench_bode_vs
|
||||
% #+caption: Bode plot of the transfer function from $V_a$ to $V_s$
|
||||
% #+RESULTS:
|
||||
% [[file:figs/apa_model_bench_bode_vs.png]]
|
||||
|
||||
|
||||
%% Bode plot of the transfer function from Va to de and da
|
||||
freqs = logspace(1, 3, 1000);
|
||||
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
plot(freqs, abs(squeeze(freqresp(Ga('de', 'Va'), freqs, 'Hz'))), 'DisplayName', 'Encoder')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $d/V_a$ [m/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
legend('location', 'southwest');
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Ga('de', 'Va'), freqs, 'Hz'))))
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:45:360);
|
||||
ylim([-180, 0])
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
|
||||
% Identification Data
|
||||
% Let's load the measured FRF from the DAC voltage to the measured encoder and to the sensor stack voltage.
|
||||
|
||||
%% Load Data
|
||||
load('meas_apa_frf.mat', 'f', 'Ts', 'enc_frf', 'iff_frf', 'apa_nums');
|
||||
|
||||
% 2DoF APA
|
||||
% Let's initialize the APA as a 2DoF model with unity sensor and actuator gains.
|
||||
|
||||
%% Initialize a 2DoF APA with Ga=Gs=1
|
||||
n_hexapod.actuator = initializeAPA(...
|
||||
'type', '2dof', ...
|
||||
'ga', 1, ...
|
||||
'gs', 1);
|
||||
|
||||
% Identification without actuator or sensor constants
|
||||
% The transfer function from $V_a$ to $V_s$, $d_e$ and $d_a$ is identified.
|
||||
|
||||
%% Input/Output definition
|
||||
clear io; io_i = 1;
|
||||
io(io_i) = linio([mdl, '/Va'], 1, 'openinput'); io_i = io_i + 1; % Actuator Voltage
|
||||
io(io_i) = linio([mdl, '/Vs'], 1, 'openoutput'); io_i = io_i + 1; % Sensor Voltage
|
||||
io(io_i) = linio([mdl, '/de'], 1, 'openoutput'); io_i = io_i + 1; % Encoder
|
||||
io(io_i) = linio([mdl, '/da'], 1, 'openoutput'); io_i = io_i + 1; % Attocube
|
||||
|
||||
%% Identification
|
||||
Gs = linearize(mdl, io, 0.0, options);
|
||||
Gs.InputName = {'Va'};
|
||||
Gs.OutputName = {'Vs', 'de', 'da'};
|
||||
|
||||
% Actuator Constant
|
||||
% Then, the actuator constant can be computed as shown in Eq. eqref:eq:actuator_constant_formula by dividing the measured DC gain of the transfer function from $V_a$ to $d_e$ by the estimated DC gain of the transfer function from $V_a$ (in truth the actuator force called $F_a$) to $d_e$ using the Simscape model.
|
||||
|
||||
%% Estimated Actuator Constant
|
||||
ga = -mean(abs(enc_frf(f>10 & f<20)))./dcgain(Gs('de', 'Va')); % [N/V]
|
||||
|
||||
% Sensor Constant
|
||||
% Similarly, the sensor constant can be estimated using Eq. eqref:eq:sensor_constant_formula.
|
||||
|
||||
|
||||
%% Estimated Sensor Constant
|
||||
gs = -mean(abs(iff_frf(f>400 & f<500)))./(ga*abs(squeeze(freqresp(Gs('Vs', 'Va'), 1e3, 'Hz')))); % [V/m]
|
||||
|
||||
% Comparison
|
||||
% Let's now initialize the APA with identified sensor and actuator constant:
|
||||
|
||||
%% Set the identified constants
|
||||
n_hexapod.actuator = initializeAPA(...
|
||||
'type', '2dof', ...
|
||||
'ga', ga, ... % Actuator gain [N/V]
|
||||
'gs', gs); % Sensor gain [V/m]
|
||||
|
||||
|
||||
|
||||
% And identify the dynamics with included constants.
|
||||
|
||||
%% Identify again the dynamics with correct Ga,Gs
|
||||
Gs = linearize(mdl, io, 0.0, options);
|
||||
Gs = Gs*exp(-Ts*s);
|
||||
Gs.InputName = {'Va'};
|
||||
Gs.OutputName = {'Vs', 'de', 'da'};
|
||||
|
||||
|
||||
|
||||
% The transfer functions from $V_a$ to $d_e$ are compared in Figure ref:fig:apa_act_constant_comp and the one from $V_a$ to $V_s$ are compared in Figure ref:fig:apa_sens_constant_comp.
|
||||
|
||||
|
||||
%% Bode plot of the transfer function from u to de
|
||||
freqs = logspace(1,4,1000);
|
||||
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(enc_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('de', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $d\mathcal{L}_m/u$ [m/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-8, 1e-3]);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(enc_frf(:,1)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('de', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:apa_act_constant_comp
|
||||
% #+caption: Comparison of the experimental data and Simscape model ($V_a$ to $d_e$)
|
||||
% #+RESULTS:
|
||||
% [[file:figs/apa_act_constant_comp.png]]
|
||||
|
||||
|
||||
%% Bode plot of the transfer function from Va to Vs (both Simscape and measured FRF)
|
||||
freqs = logspace(1,4,1000);
|
||||
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(iff_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $\tau_m/u$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-2, 1e2]);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(iff_frf(:,1)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:apa_sens_constant_comp
|
||||
% #+caption: Comparison of the experimental data and Simscape model ($V_a$ to $V_s$)
|
||||
% #+RESULTS:
|
||||
% [[file:figs/apa_sens_constant_comp.png]]
|
||||
|
||||
|
||||
%% Compare the FRF and identified dynamics from Va to Vs and da
|
||||
colors = colororder;
|
||||
|
||||
figure;
|
||||
tiledlayout(3, 2, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
plot(f, abs(enc_frf(:, 1)), 'color', [0,0,0,0.2], ...
|
||||
'DisplayName', 'FRF');
|
||||
for i = 2:length(apa_nums)
|
||||
plot(f, abs(enc_frf(:, i)), 'color', [0,0,0, 0.2], ...
|
||||
'HandleVisibility', 'off');
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('da', 'Va'), freqs, 'Hz'))), '--', ...
|
||||
'DisplayName', 'Model')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $d_a/V_a$ [m/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-8, 1e-3]);
|
||||
legend('location', 'southwest');
|
||||
|
||||
ax1b = nexttile([2,1]);
|
||||
hold on;
|
||||
plot(f, abs(iff_frf(:, i)), 'color', [0,0,0,0.2], ...
|
||||
'DisplayName', 'FRF');
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(iff_frf(:, i)), 'color', [0,0,0,0.2], ...
|
||||
'HandleVisibility', 'off');
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))), '--', ...
|
||||
'DisplayName', 'Model')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $V_s/V_a$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-2, 1e2]);
|
||||
legend('location', 'southeast');
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(enc_frf(:, i)), 'color', [0,0,0, 0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('da', 'Va'), freqs, 'Hz'))), '--')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
ax2b = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(iff_frf(:, i)), 'color', [0,0,0, 0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))), '--')
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2,ax1b,ax2b],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
% Flexible APA
|
||||
% The Simscape APA model is initialized as a flexible one with unity "constants".
|
||||
|
||||
%% Initialize the APA as a flexible body
|
||||
n_hexapod.actuator = initializeAPA(...
|
||||
'type', 'flexible', ...
|
||||
'ga', 1, ...
|
||||
'gs', 1);
|
||||
|
||||
% Identification without actuator or sensor constants
|
||||
% The dynamics from $V_a$ to $V_s$, $d_e$ and $d_a$ is identified.
|
||||
|
||||
%% Identify the dynamics
|
||||
Gs = linearize(mdl, io, 0.0, options);
|
||||
Gs.InputName = {'Va'};
|
||||
Gs.OutputName = {'Vs', 'de', 'da'};
|
||||
|
||||
% Actuator Constant
|
||||
% Then, the actuator constant can be computed as shown in Eq. eqref:eq:actuator_constant_formula:
|
||||
|
||||
%% Actuator Constant
|
||||
ga = -mean(abs(enc_frf(f>10 & f<20)))./dcgain(Gs('de', 'Va')); % [N/V]
|
||||
|
||||
% Sensor Constant
|
||||
|
||||
%% Sensor Constant
|
||||
gs = -mean(abs(iff_frf(f>400 & f<500)))./(ga*abs(squeeze(freqresp(Gs('Vs', 'Va'), 1e3, 'Hz')))); % [V/m]
|
||||
|
||||
% Comparison
|
||||
% Let's now initialize the flexible APA with identified sensor and actuator constant:
|
||||
|
||||
%% Set the identified constants
|
||||
n_hexapod.actuator = initializeAPA(...
|
||||
'type', 'flexible', ...
|
||||
'ga', ga, ... % Actuator gain [N/V]
|
||||
'gs', gs); % Sensor gain [V/m]
|
||||
|
||||
|
||||
|
||||
% And identify the dynamics with included constants.
|
||||
|
||||
%% Identify with updated constants
|
||||
Gs = linearize(mdl, io, 0.0, options);
|
||||
Gs = Gs*exp(-Ts*s);
|
||||
Gs.InputName = {'Va'};
|
||||
Gs.OutputName = {'Vs', 'de', 'da'};
|
||||
|
||||
|
||||
|
||||
% The obtained dynamics is compared with the measured one in Figures ref:fig:apa_act_constant_comp_flex and ref:fig:apa_sens_constant_comp_flex.
|
||||
|
||||
|
||||
%% Bode plot of the transfer function from V_a to d_e (both Simscape and measured FRF)
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(enc_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('de', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $d\mathcal{L}_m/u$ [m/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-9, 1e-3]);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(enc_frf(:,1)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('de', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
|
||||
|
||||
% #+name: fig:apa_act_constant_comp_flex
|
||||
% #+caption: Comparison of the experimental data and Simscape model ($u$ to $d\mathcal{L}_m$)
|
||||
% #+RESULTS:
|
||||
% [[file:figs/apa_act_constant_comp_flex.png]]
|
||||
|
||||
|
||||
%% Bode plot of the transfer function from Va to Vs (both Simscape and measured FRF)
|
||||
figure;
|
||||
tiledlayout(3, 1, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(iff_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $\tau_m/u$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-2, 1e2]);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(iff_frf(:,1)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2],'x');
|
||||
xlim([10, 2e3]);
|
||||
|
||||
% Optimize 2-DoF model to fit the experimental Data
|
||||
% <<sec:simscape_bench_apa_tune_2dof_model>>
|
||||
% The parameters of the 2DoF model presented in Section ref:sec:apa_2dof_model are now optimize such that the model best matches the measured FRF.
|
||||
|
||||
% After optimization, the following parameters are used:
|
||||
|
||||
%% Optimized parameters
|
||||
n_hexapod.actuator = initializeAPA('type', '2dof', ...
|
||||
'Ga', -32.2, ...
|
||||
'Gs', 0.088, ...
|
||||
'k', ones(6,1)*0.38e6, ...
|
||||
'ke', ones(6,1)*1.75e6, ...
|
||||
'ka', ones(6,1)*3e7, ...
|
||||
'c', ones(6,1)*1.3e2, ...
|
||||
'ce', ones(6,1)*1e1, ...
|
||||
'ca', ones(6,1)*1e1 ...
|
||||
);
|
||||
|
||||
%% Input/Output definition
|
||||
clear io; io_i = 1;
|
||||
io(io_i) = linio([mdl, '/Va'], 1, 'openinput'); io_i = io_i + 1; % Actuator Voltage
|
||||
io(io_i) = linio([mdl, '/Vs'], 1, 'openoutput'); io_i = io_i + 1; % Sensor Voltage
|
||||
io(io_i) = linio([mdl, '/de'], 1, 'openoutput'); io_i = io_i + 1; % Encoder
|
||||
|
||||
%% Identification with optimized parameters
|
||||
Gs = exp(-s*Ts)*linearize(mdl, io, 0.0, options);
|
||||
Gs.InputName = {'Va'};
|
||||
Gs.OutputName = {'Vs', 'de'};
|
||||
|
||||
|
||||
|
||||
% The dynamics is identified using the Simscape model and compared with the measured FRF in Figure ref:fig:comp_apa_plant_after_opt.
|
||||
|
||||
%% Comparison of the experimental data and Simscape Model
|
||||
freqs = 5*logspace(0, 3, 1000);
|
||||
figure;
|
||||
tiledlayout(3, 2, 'TileSpacing', 'Compact', 'Padding', 'None');
|
||||
|
||||
ax1 = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(enc_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('de', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $d_e/V_a$ [m/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-8, 1e-3]);
|
||||
|
||||
ax1b = nexttile([2,1]);
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, abs(iff_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, abs(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'log');
|
||||
ylabel('Amplitude $V_s/V_a$ [V/V]'); set(gca, 'XTickLabel',[]);
|
||||
hold off;
|
||||
ylim([1e-2, 1e2]);
|
||||
|
||||
ax2 = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(enc_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('de', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
ax2b = nexttile;
|
||||
hold on;
|
||||
for i = 1:length(apa_nums)
|
||||
plot(f, 180/pi*angle(iff_frf(:, i)), 'color', [0,0,0,0.2]);
|
||||
end
|
||||
set(gca,'ColorOrderIndex',1);
|
||||
plot(freqs, 180/pi*angle(squeeze(freqresp(Gs('Vs', 'Va'), freqs, 'Hz'))))
|
||||
hold off;
|
||||
set(gca, 'XScale', 'log'); set(gca, 'YScale', 'lin');
|
||||
xlabel('Frequency [Hz]'); ylabel('Phase [deg]');
|
||||
hold off;
|
||||
yticks(-360:90:360); ylim([-180, 180]);
|
||||
|
||||
linkaxes([ax1,ax2,ax1b,ax2b],'x');
|
||||
xlim([10, 2e3]);
|
BIN
matlab/test_apa_simscape.slx
Normal file
BIN
matlab/test_apa_simscape.slx
Normal file
Binary file not shown.
@ -621,9 +621,9 @@ It is however quite interesting that there is a factor $\approx \sqrt{2}$ betwee
|
||||
|
||||
** Conclusion :ignore:
|
||||
|
||||
* Dynamical measurements - APA
|
||||
* Dynamical measurements
|
||||
:PROPERTIES:
|
||||
:header-args:matlab+: :tangle matlab/2_test_apa_dynamics.m
|
||||
:header-args:matlab+: :tangle matlab/test_apa_2_dynamics.m
|
||||
:END:
|
||||
<<sec:test_apa_dynamics>>
|
||||
|
||||
@ -1218,7 +1218,7 @@ for i = 1:length(i_kept)
|
||||
end
|
||||
#+end_src
|
||||
|
||||
The identified dynamics are then fitted by second order transfer functions using the "Vector Fitting" toolbox [[cite:&gustavsen99_ration_approx_frequen_domain_respon]].
|
||||
The identified dynamics are then fitted by second order transfer functions.
|
||||
The comparison between the identified damped dynamics and the fitted second order transfer functions is done in Figure ref:fig:test_apa_identified_damped_plants for different gains $g$.
|
||||
It is clear that large amount of damping is added when the gain is increased and that the frequency of the pole is shifted to lower frequencies.
|
||||
|
||||
@ -1338,9 +1338,9 @@ So far, all the measured FRF are showing the dynamical behavior that was expecte
|
||||
#+end_important
|
||||
|
||||
|
||||
* TODO Test Bench APA300ML - Simscape Model
|
||||
* Simscape Model
|
||||
:PROPERTIES:
|
||||
:header-args:matlab+: :tangle matlab/3_test_apa_simscape.m
|
||||
:header-args:matlab+: :tangle matlab/test_apa_3_simscape.m
|
||||
:END:
|
||||
<<sec:test_apa_simscape>>
|
||||
** Introduction :ignore:
|
||||
@ -1366,35 +1366,24 @@ After the transfer functions are extracted from the model (Section ref:sec:simsc
|
||||
<<matlab-init>>
|
||||
#+end_src
|
||||
|
||||
#+begin_src matlab :tangle no
|
||||
%% Add useful folders to the path
|
||||
addpath('matlab/');
|
||||
addpath('matlab/STEPS/');
|
||||
addpath('matlab/mat/');
|
||||
addpath('matlab/src/');
|
||||
#+begin_src matlab :tangle no :noweb yes
|
||||
<<m-init-path>>
|
||||
#+end_src
|
||||
|
||||
#+begin_src matlab :eval no
|
||||
%% Add useful folders to the path
|
||||
addpath('STEPS/');
|
||||
addpath('mat/');
|
||||
addpath('src/');
|
||||
#+begin_src matlab :eval no :noweb yes
|
||||
<<m-init-path-tangle>>
|
||||
#+end_src
|
||||
|
||||
#+begin_src matlab
|
||||
%% Frequency vector used for many plots
|
||||
freqs = 2*logspace(0, 3, 1000);
|
||||
#+begin_src matlab :tangle no :noweb yes
|
||||
<<m-init-path-simscape>>
|
||||
#+end_src
|
||||
|
||||
#+begin_src matlab
|
||||
%% Open Simscape Model
|
||||
options = linearizeOptions;
|
||||
options.SampleTime = 0;
|
||||
#+begin_src matlab :eval no :noweb yes
|
||||
<<m-init-path-simscape-tangle>>
|
||||
#+end_src
|
||||
|
||||
% Name of the Simulink File
|
||||
mdl = 'test_apa300ml';
|
||||
|
||||
open(mdl)
|
||||
#+begin_src matlab :noweb yes
|
||||
<<m-init-other>>
|
||||
#+end_src
|
||||
|
||||
** First Identification
|
||||
@ -1421,8 +1410,12 @@ io(io_i) = linio([mdl, '/Va'], 1, 'openinput'); io_i = io_i + 1; % DAC Voltage
|
||||
io(io_i) = linio([mdl, '/Vs'], 1, 'openoutput'); io_i = io_i + 1; % Sensor Voltage
|
||||
io(io_i) = linio([mdl, '/de'], 1, 'openoutput'); io_i = io_i + 1; % Encoder
|
||||
|
||||
%% Linearization options
|
||||
opts = linearizeOptions;
|
||||
opts.SampleTime = 0;
|
||||
|
||||
%% Run the linearization
|
||||
Ga = linearize(mdl, io, 0.0, options);
|
||||
Ga = linearize(mdl, io, 0.0, opts);
|
||||
Ga.InputName = {'Va'};
|
||||
Ga.OutputName = {'Vs', 'de', 'da'};
|
||||
#+end_src
|
||||
@ -3029,6 +3022,25 @@ addpath('./src/'); % Path for scripts
|
||||
addpath('./mat/'); % Path for data
|
||||
#+END_SRC
|
||||
|
||||
** Initialize Simscape
|
||||
#+NAME: m-init-path-simscape
|
||||
#+BEGIN_SRC matlab
|
||||
addpath('./matlab/STEPS/'); % Path for Simscape Model
|
||||
|
||||
%% Open Simscape Model
|
||||
mdl = 'test_apa_simscape'; % Name of the Simulink File
|
||||
open(mdl); % Open Simscape Model
|
||||
#+END_SRC
|
||||
|
||||
#+NAME: m-init-path-simscape-tangle
|
||||
#+BEGIN_SRC matlab
|
||||
addpath('./STEPS/'); % Path for Simscape Model
|
||||
|
||||
%% Open Simscape Model
|
||||
mdl = 'test_apa_simscape'; % Name of the Simulink File
|
||||
open(mdl); % Open Simscape Model
|
||||
#+END_SRC
|
||||
|
||||
** Initialize other elements
|
||||
#+NAME: m-init-other
|
||||
#+BEGIN_SRC matlab
|
||||
|
Loading…
Reference in New Issue
Block a user