Change two damping values
Before Width: | Height: | Size: 91 KiB After Width: | Height: | Size: 91 KiB |
Before Width: | Height: | Size: 80 KiB After Width: | Height: | Size: 80 KiB |
Before Width: | Height: | Size: 92 KiB After Width: | Height: | Size: 93 KiB |
Before Width: | Height: | Size: 84 KiB After Width: | Height: | Size: 84 KiB |
@ -32,11 +32,11 @@ freqs = 5*logspace(0, 3, 1000);
|
|||||||
|
|
||||||
% Tuning of the APA model :ignore:
|
% Tuning of the APA model :ignore:
|
||||||
|
|
||||||
% 9 parameters ($m$, $k_1$, $c_1$, $k_e$, $c_e$, $k_a$, $c_a$, $g_s$ and $g_a$) have to be tuned such that the dynamics of the model (Figure ref:fig:test_apa_2dof_model_Simscape) well represents the identified dynamics in Section ref:sec:test_apa_dynamics.
|
% 9 parameters ($m$, $k_1$, $c_1$, $k_e$, $c_e$, $k_a$, $c_a$, $g_s$ and $g_a$) have to be tuned such that the dynamics of the model (Figure ref:fig:test_apa_2dof_model_simscape) well represents the identified dynamics in Section ref:sec:test_apa_dynamics.
|
||||||
|
|
||||||
% #+name: fig:test_apa_2dof_model_Simscape
|
% #+name: fig:test_apa_2dof_model_simscape
|
||||||
% #+caption: Schematic of the two degrees-of-freedom model of the APA300ML with input $V_a$ and outputs $d_e$ and $V_s$
|
% #+caption: Schematic of the two degrees-of-freedom model of the APA300ML with input $V_a$ and outputs $d_e$ and $V_s$
|
||||||
% [[file:figs/test_apa_2dof_model_Simscape.png]]
|
% [[file:figs/test_apa_2dof_model_simscape.png]]
|
||||||
|
|
||||||
|
|
||||||
%% Stiffness values for the 2DoF APA model
|
%% Stiffness values for the 2DoF APA model
|
||||||
@ -50,8 +50,8 @@ ka = 1.5*(ktot-k1); % Stiffness of the (two) actuator stacks [N/m]
|
|||||||
ke = 2*ka; % Stiffness of the Sensor stack [N/m]
|
ke = 2*ka; % Stiffness of the Sensor stack [N/m]
|
||||||
|
|
||||||
%% Damping values for the 2DoF APA model
|
%% Damping values for the 2DoF APA model
|
||||||
c1 = 20; % Damping for the Shell [N/(m/s)]
|
c1 = 5; % Damping for the Shell [N/(m/s)]
|
||||||
ca = 100; % Damping of the actuators stacks [N/(m/s)]
|
ca = 50; % Damping of the actuators stacks [N/(m/s)]
|
||||||
ce = 2*ca; % Damping of the sensor stack [N/(m/s)]
|
ce = 2*ca; % Damping of the sensor stack [N/(m/s)]
|
||||||
|
|
||||||
%% Estimation ot the sensor and actuator sensitivities
|
%% Estimation ot the sensor and actuator sensitivities
|
||||||
@ -69,7 +69,7 @@ n_hexapod.actuator = initializeAPA(...
|
|||||||
'Gs', 1 ... % Sensor constant [V/m]
|
'Gs', 1 ... % Sensor constant [V/m]
|
||||||
);
|
);
|
||||||
|
|
||||||
c_granite = 0; % Do not take into account damping added by the air bearing
|
c_granite = 50; % Do not take into account damping added by the air bearing
|
||||||
|
|
||||||
% Run the linearization
|
% Run the linearization
|
||||||
G_norm = linearize(mdl, io, 0.0, opts);
|
G_norm = linearize(mdl, io, 0.0, opts);
|
||||||
|
@ -44,7 +44,7 @@ n_hexapod.actuator = initializeAPA(...
|
|||||||
'ga', 1, ...
|
'ga', 1, ...
|
||||||
'gs', 1);
|
'gs', 1);
|
||||||
|
|
||||||
c_granite = 100; % Rought estimation of the damping added by the air bearing
|
c_granite = 50; % Rought estimation of the damping added by the air bearing
|
||||||
|
|
||||||
% Identify the dynamics
|
% Identify the dynamics
|
||||||
G_norm = linearize(mdl, io, 0.0, opts);
|
G_norm = linearize(mdl, io, 0.0, opts);
|
||||||
|
@ -1396,11 +1396,11 @@ Such a simple model has some limitations:
|
|||||||
|
|
||||||
**** Tuning of the APA model :ignore:
|
**** Tuning of the APA model :ignore:
|
||||||
|
|
||||||
9 parameters ($m$, $k_1$, $c_1$, $k_e$, $c_e$, $k_a$, $c_a$, $g_s$ and $g_a$) have to be tuned such that the dynamics of the model (Figure ref:fig:test_apa_2dof_model_Simscape) well represents the identified dynamics in Section ref:sec:test_apa_dynamics.
|
9 parameters ($m$, $k_1$, $c_1$, $k_e$, $c_e$, $k_a$, $c_a$, $g_s$ and $g_a$) have to be tuned such that the dynamics of the model (Figure ref:fig:test_apa_2dof_model_simscape) well represents the identified dynamics in Section ref:sec:test_apa_dynamics.
|
||||||
|
|
||||||
#+name: fig:test_apa_2dof_model_Simscape
|
#+name: fig:test_apa_2dof_model_simscape
|
||||||
#+caption: Schematic of the two degrees-of-freedom model of the APA300ML with input $V_a$ and outputs $d_e$ and $V_s$
|
#+caption: Schematic of the two degrees-of-freedom model of the APA300ML with input $V_a$ and outputs $d_e$ and $V_s$
|
||||||
[[file:figs/test_apa_2dof_model_Simscape.png]]
|
[[file:figs/test_apa_2dof_model_simscape.png]]
|
||||||
|
|
||||||
#+begin_src matlab
|
#+begin_src matlab
|
||||||
%% Stiffness values for the 2DoF APA model
|
%% Stiffness values for the 2DoF APA model
|
||||||
@ -1414,8 +1414,8 @@ ka = 1.5*(ktot-k1); % Stiffness of the (two) actuator stacks [N/m]
|
|||||||
ke = 2*ka; % Stiffness of the Sensor stack [N/m]
|
ke = 2*ka; % Stiffness of the Sensor stack [N/m]
|
||||||
|
|
||||||
%% Damping values for the 2DoF APA model
|
%% Damping values for the 2DoF APA model
|
||||||
c1 = 20; % Damping for the Shell [N/(m/s)]
|
c1 = 5; % Damping for the Shell [N/(m/s)]
|
||||||
ca = 100; % Damping of the actuators stacks [N/(m/s)]
|
ca = 50; % Damping of the actuators stacks [N/(m/s)]
|
||||||
ce = 2*ca; % Damping of the sensor stack [N/(m/s)]
|
ce = 2*ca; % Damping of the sensor stack [N/(m/s)]
|
||||||
#+end_src
|
#+end_src
|
||||||
|
|
||||||
@ -1435,7 +1435,7 @@ n_hexapod.actuator = initializeAPA(...
|
|||||||
'Gs', 1 ... % Sensor constant [V/m]
|
'Gs', 1 ... % Sensor constant [V/m]
|
||||||
);
|
);
|
||||||
|
|
||||||
c_granite = 0; % Do not take into account damping added by the air bearing
|
c_granite = 50; % Do not take into account damping added by the air bearing
|
||||||
|
|
||||||
% Run the linearization
|
% Run the linearization
|
||||||
G_norm = linearize(mdl, io, 0.0, opts);
|
G_norm = linearize(mdl, io, 0.0, opts);
|
||||||
@ -1460,7 +1460,7 @@ First, the mass $m$ supported by the APA300ML can be estimated from the geometry
|
|||||||
Both methods lead to an estimated mass of $m = 5.7\,\text{kg}$.
|
Both methods lead to an estimated mass of $m = 5.7\,\text{kg}$.
|
||||||
|
|
||||||
Then, the axial stiffness of the shell was estimated at $k_1 = 0.38\,N/\mu m$ in Section ref:ssec:test_apa_meas_dynamics from the frequency of the anti-resonance seen on Figure ref:fig:test_apa_frf_force.
|
Then, the axial stiffness of the shell was estimated at $k_1 = 0.38\,N/\mu m$ in Section ref:ssec:test_apa_meas_dynamics from the frequency of the anti-resonance seen on Figure ref:fig:test_apa_frf_force.
|
||||||
Similarly, $c_1$ can be estimated from the damping ratio of the same anti-resonance and is found to be close to $20\,Ns/m$.
|
Similarly, $c_1$ can be estimated from the damping ratio of the same anti-resonance and is found to be close to $5\,Ns/m$.
|
||||||
|
|
||||||
Then, it is reasonable to assume that the sensor stacks and the two actuator stacks have identical mechanical characteristics[fn:5].
|
Then, it is reasonable to assume that the sensor stacks and the two actuator stacks have identical mechanical characteristics[fn:5].
|
||||||
Therefore, we have $k_e = 2 k_a$ and $c_e = 2 c_a$ as the actuator stack is composed of two stacks in series.
|
Therefore, we have $k_e = 2 k_a$ and $c_e = 2 c_a$ as the actuator stack is composed of two stacks in series.
|
||||||
@ -1477,11 +1477,11 @@ Knowing from eqref:eq:test_apa_tot_stiffness that the total stiffness is $k_{\te
|
|||||||
\end{equation}
|
\end{equation}
|
||||||
|
|
||||||
Then, $c_a$ (and therefore $c_e = 2 c_a$) can be tuned to match the damping ratio of the identified resonance.
|
Then, $c_a$ (and therefore $c_e = 2 c_a$) can be tuned to match the damping ratio of the identified resonance.
|
||||||
$c_a = 100\,Ns/m$ and $c_e = 200\,Ns/m$ are obtained.
|
$c_a = 50\,Ns/m$ and $c_e = 100\,Ns/m$ are obtained.
|
||||||
|
|
||||||
In the last step, $g_s$ and $g_a$ can be tuned to match the gain of the identified transfer functions.
|
In the last step, $g_s$ and $g_a$ can be tuned to match the gain of the identified transfer functions.
|
||||||
|
|
||||||
The obtained parameters of the model shown in Figure ref:fig:test_apa_2dof_model_Simscape are summarized in Table ref:tab:test_apa_2dof_parameters.
|
The obtained parameters of the model shown in Figure ref:fig:test_apa_2dof_model_simscape are summarized in Table ref:tab:test_apa_2dof_parameters.
|
||||||
|
|
||||||
#+name: tab:test_apa_2dof_parameters
|
#+name: tab:test_apa_2dof_parameters
|
||||||
#+caption: Summary of the obtained parameters for the 2 DoF APA300ML model
|
#+caption: Summary of the obtained parameters for the 2 DoF APA300ML model
|
||||||
@ -1493,9 +1493,9 @@ The obtained parameters of the model shown in Figure ref:fig:test_apa_2dof_model
|
|||||||
| $k_1$ | $0.38\,N/\mu m$ |
|
| $k_1$ | $0.38\,N/\mu m$ |
|
||||||
| $k_e$ | $5.0\, N/\mu m$ |
|
| $k_e$ | $5.0\, N/\mu m$ |
|
||||||
| $k_a$ | $2.5\,N/\mu m$ |
|
| $k_a$ | $2.5\,N/\mu m$ |
|
||||||
| $c_1$ | $20\,Ns/m$ |
|
| $c_1$ | $5\,Ns/m$ |
|
||||||
| $c_e$ | $200\,Ns/m$ |
|
| $c_e$ | $100\,Ns/m$ |
|
||||||
| $c_a$ | $100\,Ns/m$ |
|
| $c_a$ | $50\,Ns/m$ |
|
||||||
| $g_a$ | $-2.58\,N/V$ |
|
| $g_a$ | $-2.58\,N/V$ |
|
||||||
| $g_s$ | $0.46\,V/\mu m$ |
|
| $g_s$ | $0.46\,V/\mu m$ |
|
||||||
|
|
||||||
@ -1632,7 +1632,7 @@ exportFig('figs/test_apa_2dof_comp_frf_force.pdf', 'width', 'half', 'height', 't
|
|||||||
**** Introduction :ignore:
|
**** Introduction :ignore:
|
||||||
In this section, a /super element/ of the APA300ML is computed using a finite element software[fn:11].
|
In this section, a /super element/ of the APA300ML is computed using a finite element software[fn:11].
|
||||||
It is then imported into Simscape (in the form of a stiffness matrix and a mass matrix) and included in the same model that was used in ref:sec:test_apa_model_2dof.
|
It is then imported into Simscape (in the form of a stiffness matrix and a mass matrix) and included in the same model that was used in ref:sec:test_apa_model_2dof.
|
||||||
This procedure is illustrated in Figure ref:fig:test_apa_super_element_Simscape.
|
This procedure is illustrated in Figure ref:fig:test_apa_super_element_simscape.
|
||||||
Several /remote points/ are defined in the finite element model (here illustrated by colorful planes and numbers from =1= to =5=) and are then made accessible in the Simscape model as shown at the right by the "frames" =F1= to =F5=.
|
Several /remote points/ are defined in the finite element model (here illustrated by colorful planes and numbers from =1= to =5=) and are then made accessible in the Simscape model as shown at the right by the "frames" =F1= to =F5=.
|
||||||
|
|
||||||
For the APA300ML /super element/, 5 /remote points/ are defined.
|
For the APA300ML /super element/, 5 /remote points/ are defined.
|
||||||
@ -1640,10 +1640,10 @@ Two /remote points/ (=1= and =2=) are fixed to the top and bottom mechanical int
|
|||||||
Two /remote points/ (=3= and =4=) are located across two piezoelectric stacks and are used to apply internal forces representing the actuator stacks.
|
Two /remote points/ (=3= and =4=) are located across two piezoelectric stacks and are used to apply internal forces representing the actuator stacks.
|
||||||
Finally, two /remote points/ (=4= and =4=) are located across the third piezoelectric stack, and will be used to measured the strain of the sensor stack.
|
Finally, two /remote points/ (=4= and =4=) are located across the third piezoelectric stack, and will be used to measured the strain of the sensor stack.
|
||||||
|
|
||||||
#+name: fig:test_apa_super_element_Simscape
|
#+name: fig:test_apa_super_element_simscape
|
||||||
#+attr_latex: :width 1.0\linewidth
|
#+attr_latex: :width 1.0\linewidth
|
||||||
#+caption: Finite Element Model of the APA300ML with "remotes points" on the left. Simscape model with included "Reduced Order Flexible Solid" on the right.
|
#+caption: Finite Element Model of the APA300ML with "remotes points" on the left. Simscape model with included "Reduced Order Flexible Solid" on the right.
|
||||||
[[file:figs/test_apa_super_element_Simscape.png]]
|
[[file:figs/test_apa_super_element_simscape.png]]
|
||||||
|
|
||||||
**** Matlab Init :noexport:ignore:
|
**** Matlab Init :noexport:ignore:
|
||||||
#+begin_src matlab :tangle no :exports none :results silent :noweb yes :var current_dir=(file-name-directory buffer-file-name)
|
#+begin_src matlab :tangle no :exports none :results silent :noweb yes :var current_dir=(file-name-directory buffer-file-name)
|
||||||
@ -1699,7 +1699,7 @@ n_hexapod.actuator = initializeAPA(...
|
|||||||
'ga', 1, ...
|
'ga', 1, ...
|
||||||
'gs', 1);
|
'gs', 1);
|
||||||
|
|
||||||
c_granite = 100; % Rought estimation of the damping added by the air bearing
|
c_granite = 50; % Rought estimation of the damping added by the air bearing
|
||||||
|
|
||||||
% Identify the dynamics
|
% Identify the dynamics
|
||||||
G_norm = linearize(mdl, io, 0.0, opts);
|
G_norm = linearize(mdl, io, 0.0, opts);
|
||||||
|
@ -1,4 +1,4 @@
|
|||||||
% Created 2024-04-30 Tue 17:24
|
% Created 2024-10-26 Sat 12:10
|
||||||
% Intended LaTeX compiler: pdflatex
|
% Intended LaTeX compiler: pdflatex
|
||||||
\documentclass[a4paper, 10pt, DIV=12, parskip=full, bibliography=totoc]{scrreprt}
|
\documentclass[a4paper, 10pt, DIV=12, parskip=full, bibliography=totoc]{scrreprt}
|
||||||
|
|
||||||
@ -31,7 +31,7 @@
|
|||||||
pdftitle={Test Bench - Amplified Piezoelectric Actuator},
|
pdftitle={Test Bench - Amplified Piezoelectric Actuator},
|
||||||
pdfkeywords={},
|
pdfkeywords={},
|
||||||
pdfsubject={},
|
pdfsubject={},
|
||||||
pdfcreator={Emacs 29.3 (Org mode 9.6)},
|
pdfcreator={Emacs 29.4 (Org mode 9.6)},
|
||||||
pdflang={English}}
|
pdflang={English}}
|
||||||
\usepackage{biblatex}
|
\usepackage{biblatex}
|
||||||
|
|
||||||
@ -553,19 +553,19 @@ Such a simple model has some limitations:
|
|||||||
\caption{\label{fig:test_apa_2dof_model}Schematic of the two degrees-of-freedom model of the APA300ML, adapted from \cite{souleille18_concep_activ_mount_space_applic}}
|
\caption{\label{fig:test_apa_2dof_model}Schematic of the two degrees-of-freedom model of the APA300ML, adapted from \cite{souleille18_concep_activ_mount_space_applic}}
|
||||||
\end{figure}
|
\end{figure}
|
||||||
|
|
||||||
9 parameters (\(m\), \(k_1\), \(c_1\), \(k_e\), \(c_e\), \(k_a\), \(c_a\), \(g_s\) and \(g_a\)) have to be tuned such that the dynamics of the model (Figure \ref{fig:test_apa_2dof_model_Simscape}) well represents the identified dynamics in Section \ref{sec:test_apa_dynamics}.
|
9 parameters (\(m\), \(k_1\), \(c_1\), \(k_e\), \(c_e\), \(k_a\), \(c_a\), \(g_s\) and \(g_a\)) have to be tuned such that the dynamics of the model (Figure \ref{fig:test_apa_2dof_model_simscape}) well represents the identified dynamics in Section \ref{sec:test_apa_dynamics}.
|
||||||
|
|
||||||
\begin{figure}[htbp]
|
\begin{figure}[htbp]
|
||||||
\centering
|
\centering
|
||||||
\includegraphics[scale=1]{figs/test_apa_2dof_model_Simscape.png}
|
\includegraphics[scale=1]{figs/test_apa_2dof_model_simscape.png}
|
||||||
\caption{\label{fig:test_apa_2dof_model_Simscape}Schematic of the two degrees-of-freedom model of the APA300ML with input \(V_a\) and outputs \(d_e\) and \(V_s\)}
|
\caption{\label{fig:test_apa_2dof_model_simscape}Schematic of the two degrees-of-freedom model of the APA300ML with input \(V_a\) and outputs \(d_e\) and \(V_s\)}
|
||||||
\end{figure}
|
\end{figure}
|
||||||
|
|
||||||
First, the mass \(m\) supported by the APA300ML can be estimated from the geometry and density of the different parts or by directly measuring it using a precise weighing scale.
|
First, the mass \(m\) supported by the APA300ML can be estimated from the geometry and density of the different parts or by directly measuring it using a precise weighing scale.
|
||||||
Both methods lead to an estimated mass of \(m = 5.7\,\text{kg}\).
|
Both methods lead to an estimated mass of \(m = 5.7\,\text{kg}\).
|
||||||
|
|
||||||
Then, the axial stiffness of the shell was estimated at \(k_1 = 0.38\,N/\mu m\) in Section \ref{ssec:test_apa_meas_dynamics} from the frequency of the anti-resonance seen on Figure \ref{fig:test_apa_frf_force}.
|
Then, the axial stiffness of the shell was estimated at \(k_1 = 0.38\,N/\mu m\) in Section \ref{ssec:test_apa_meas_dynamics} from the frequency of the anti-resonance seen on Figure \ref{fig:test_apa_frf_force}.
|
||||||
Similarly, \(c_1\) can be estimated from the damping ratio of the same anti-resonance and is found to be close to \(20\,Ns/m\).
|
Similarly, \(c_1\) can be estimated from the damping ratio of the same anti-resonance and is found to be close to \(5\,Ns/m\).
|
||||||
|
|
||||||
Then, it is reasonable to assume that the sensor stacks and the two actuator stacks have identical mechanical characteristics\footnote{Note that this is not completely correct as it was shown in Section \ref{ssec:test_apa_stiffness} that the electrical boundaries of the piezoelectric stack impacts its stiffness and that the sensor stack is almost open-circuited while the actuator stacks are almost short-circuited.}.
|
Then, it is reasonable to assume that the sensor stacks and the two actuator stacks have identical mechanical characteristics\footnote{Note that this is not completely correct as it was shown in Section \ref{ssec:test_apa_stiffness} that the electrical boundaries of the piezoelectric stack impacts its stiffness and that the sensor stack is almost open-circuited while the actuator stacks are almost short-circuited.}.
|
||||||
Therefore, we have \(k_e = 2 k_a\) and \(c_e = 2 c_a\) as the actuator stack is composed of two stacks in series.
|
Therefore, we have \(k_e = 2 k_a\) and \(c_e = 2 c_a\) as the actuator stack is composed of two stacks in series.
|
||||||
@ -582,11 +582,11 @@ Knowing from \eqref{eq:test_apa_tot_stiffness} that the total stiffness is \(k_{
|
|||||||
\end{equation}
|
\end{equation}
|
||||||
|
|
||||||
Then, \(c_a\) (and therefore \(c_e = 2 c_a\)) can be tuned to match the damping ratio of the identified resonance.
|
Then, \(c_a\) (and therefore \(c_e = 2 c_a\)) can be tuned to match the damping ratio of the identified resonance.
|
||||||
\(c_a = 100\,Ns/m\) and \(c_e = 200\,Ns/m\) are obtained.
|
\(c_a = 50\,Ns/m\) and \(c_e = 100\,Ns/m\) are obtained.
|
||||||
|
|
||||||
In the last step, \(g_s\) and \(g_a\) can be tuned to match the gain of the identified transfer functions.
|
In the last step, \(g_s\) and \(g_a\) can be tuned to match the gain of the identified transfer functions.
|
||||||
|
|
||||||
The obtained parameters of the model shown in Figure \ref{fig:test_apa_2dof_model_Simscape} are summarized in Table \ref{tab:test_apa_2dof_parameters}.
|
The obtained parameters of the model shown in Figure \ref{fig:test_apa_2dof_model_simscape} are summarized in Table \ref{tab:test_apa_2dof_parameters}.
|
||||||
|
|
||||||
\begin{table}[htbp]
|
\begin{table}[htbp]
|
||||||
\centering
|
\centering
|
||||||
@ -598,9 +598,9 @@ The obtained parameters of the model shown in Figure \ref{fig:test_apa_2dof_mode
|
|||||||
\(k_1\) & \(0.38\,N/\mu m\)\\
|
\(k_1\) & \(0.38\,N/\mu m\)\\
|
||||||
\(k_e\) & \(5.0\, N/\mu m\)\\
|
\(k_e\) & \(5.0\, N/\mu m\)\\
|
||||||
\(k_a\) & \(2.5\,N/\mu m\)\\
|
\(k_a\) & \(2.5\,N/\mu m\)\\
|
||||||
\(c_1\) & \(20\,Ns/m\)\\
|
\(c_1\) & \(5\,Ns/m\)\\
|
||||||
\(c_e\) & \(200\,Ns/m\)\\
|
\(c_e\) & \(100\,Ns/m\)\\
|
||||||
\(c_a\) & \(100\,Ns/m\)\\
|
\(c_a\) & \(50\,Ns/m\)\\
|
||||||
\(g_a\) & \(-2.58\,N/V\)\\
|
\(g_a\) & \(-2.58\,N/V\)\\
|
||||||
\(g_s\) & \(0.46\,V/\mu m\)\\
|
\(g_s\) & \(0.46\,V/\mu m\)\\
|
||||||
\bottomrule
|
\bottomrule
|
||||||
@ -634,7 +634,7 @@ This indicates that this model represents well the axial dynamics of the APA300M
|
|||||||
\label{sec:test_apa_model_flexible}
|
\label{sec:test_apa_model_flexible}
|
||||||
In this section, a \emph{super element} of the APA300ML is computed using a finite element software\footnote{Ansys\textsuperscript{\textregistered} was used}.
|
In this section, a \emph{super element} of the APA300ML is computed using a finite element software\footnote{Ansys\textsuperscript{\textregistered} was used}.
|
||||||
It is then imported into Simscape (in the form of a stiffness matrix and a mass matrix) and included in the same model that was used in \ref{sec:test_apa_model_2dof}.
|
It is then imported into Simscape (in the form of a stiffness matrix and a mass matrix) and included in the same model that was used in \ref{sec:test_apa_model_2dof}.
|
||||||
This procedure is illustrated in Figure \ref{fig:test_apa_super_element_Simscape}.
|
This procedure is illustrated in Figure \ref{fig:test_apa_super_element_simscape}.
|
||||||
Several \emph{remote points} are defined in the finite element model (here illustrated by colorful planes and numbers from \texttt{1} to \texttt{5}) and are then made accessible in the Simscape model as shown at the right by the ``frames'' \texttt{F1} to \texttt{F5}.
|
Several \emph{remote points} are defined in the finite element model (here illustrated by colorful planes and numbers from \texttt{1} to \texttt{5}) and are then made accessible in the Simscape model as shown at the right by the ``frames'' \texttt{F1} to \texttt{F5}.
|
||||||
|
|
||||||
For the APA300ML \emph{super element}, 5 \emph{remote points} are defined.
|
For the APA300ML \emph{super element}, 5 \emph{remote points} are defined.
|
||||||
@ -644,8 +644,8 @@ Finally, two \emph{remote points} (\texttt{4} and \texttt{4}) are located across
|
|||||||
|
|
||||||
\begin{figure}[htbp]
|
\begin{figure}[htbp]
|
||||||
\centering
|
\centering
|
||||||
\includegraphics[scale=1,width=1.0\linewidth]{figs/test_apa_super_element_Simscape.png}
|
\includegraphics[scale=1,width=1.0\linewidth]{figs/test_apa_super_element_simscape.png}
|
||||||
\caption{\label{fig:test_apa_super_element_Simscape}Finite Element Model of the APA300ML with ``remotes points'' on the left. Simscape model with included ``Reduced Order Flexible Solid'' on the right.}
|
\caption{\label{fig:test_apa_super_element_simscape}Finite Element Model of the APA300ML with ``remotes points'' on the left. Simscape model with included ``Reduced Order Flexible Solid'' on the right.}
|
||||||
\end{figure}
|
\end{figure}
|
||||||
|
|
||||||
\paragraph{Identification of the Actuator and Sensor constants}
|
\paragraph{Identification of the Actuator and Sensor constants}
|
||||||
|