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< / div > < div id = "content" >
< h1 class = "title" > Study of the Flexible Joints< / h1 >
< div id = "table-of-contents" >
< h2 > Table of Contents< / h2 >
< div id = "text-table-of-contents" >
< ul >
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< li > < a href = "#org157c72f" > 1. Bending and Torsional Stiffness< / a >
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< ul >
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< li > < a href = "#org19fa00c" > 1.1. Initialization< / a > < / li >
< li > < a href = "#orgc66d5ef" > 1.2. Realistic Bending Stiffness Values< / a >
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< ul >
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< li > < a href = "#org7f86aa6" > 1.2.1. Direct Velocity Feedback< / a > < / li >
< li > < a href = "#orgd763ab8" > 1.2.2. Primary Plant< / a > < / li >
< li > < a href = "#org34d48fd" > 1.2.3. Conclusion< / a > < / li >
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< / ul >
< / li >
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< li > < a href = "#org2383b0a" > 1.3. Parametric Study< / a >
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< ul >
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< li > < a href = "#org0b2ea81" > 1.3.1. Direct Velocity Feedback< / a > < / li >
< li > < a href = "#org4bcbd52" > 1.3.2. Primary Control< / a > < / li >
< li > < a href = "#orgd481cbd" > 1.3.3. Conclusion< / a > < / li >
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< / ul >
< / li >
< / ul >
< / li >
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< li > < a href = "#org122af58" > 2. Axial Stiffness< / a >
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< ul >
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< li > < a href = "#orgbd421fd" > 2.1. Realistic Translation Stiffness Values< / a >
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< ul >
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< li > < a href = "#org7e915de" > 2.1.1. Initialization< / a > < / li >
< li > < a href = "#org484b32d" > 2.1.2. Direct Velocity Feedback< / a > < / li >
< li > < a href = "#org4c02123" > 2.1.3. Primary Plant< / a > < / li >
< li > < a href = "#org8aa50f5" > 2.1.4. Conclusion< / a > < / li >
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< / ul >
< / li >
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< li > < a href = "#orge0a9c34" > 2.2. Parametric study< / a >
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< ul >
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< li > < a href = "#org564cc95" > 2.2.1. Direct Velocity Feedback< / a > < / li >
< li > < a href = "#orgc1721b8" > 2.2.2. Primary Control< / a > < / li >
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< / ul >
< / li >
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< li > < a href = "#org13f48c9" > 2.3. Conclusion< / a > < / li >
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< / ul >
< / li >
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< li > < a href = "#org5519f74" > 3. Conclusion< / a > < / li >
< li > < a href = "#org358d063" > 4. Designed Flexible Joints< / a >
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< ul >
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< li > < a href = "#org1148778" > 4.1. Initialization< / a > < / li >
< li > < a href = "#orgd889755" > 4.2. Direct Velocity Feedback< / a > < / li >
< li > < a href = "#org12972b2" > 4.3. Integral Force Feedback< / a > < / li >
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< / ul >
< / li >
< / ul >
< / div >
< / div >
< p >
In this document is studied the effect of the mechanical behavior of the flexible joints that are located the extremities of each nano-hexapod’ s legs.
< / p >
< p >
Ideally, we want the x and y rotations to be free and all the translations to be blocked.
However, this is never the case and be have to consider:
< / p >
< ul class = "org-ul" >
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< li > Finite bending stiffnesses (Section < a href = "#org27b9411" > 1< / a > )< / li >
< li > Axial stiffness in the direction of the legs (Section < a href = "#org7789cf6" > 2< / a > )< / li >
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< / ul >
< p >
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This may impose some limitations, also, the goal is to specify the required joints stiffnesses (summarized in Section < a href = "#org8e0b118" > 3< / a > ).
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< / p >
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< div id = "outline-container-org157c72f" class = "outline-2" >
< h2 id = "org157c72f" > < span class = "section-number-2" > 1< / span > Bending and Torsional Stiffness< / h2 >
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< div class = "outline-text-2" id = "text-1" >
< p >
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< a id = "org27b9411" > < / a >
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< / p >
< p >
In this section, we wish to study the effect of the rotation flexibility of the nano-hexapod joints.
< / p >
< / div >
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< div id = "outline-container-org19fa00c" class = "outline-3" >
< h3 id = "org19fa00c" > < span class = "section-number-3" > 1.1< / span > Initialization< / h3 >
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< div class = "outline-text-3" id = "text-1-1" >
< p >
Let’ s initialize all the stages with default parameters.
< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > initializeGround();
initializeGranite();
initializeTy();
initializeRy();
initializeRz();
initializeMicroHexapod();
initializeAxisc();
initializeMirror();
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< / pre >
< / div >
< p >
Let’ s consider the heaviest mass which should we the most problematic with it comes to the flexible joints.
< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > initializeSample(< span class = "org-string" > 'mass'< / span > , 50, < span class = "org-string" > 'freq'< / span > , 200< span class = "org-type" > *< / span > ones(6,1));
initializeReferences(< span class = "org-string" > 'Rz_type'< / span > , < span class = "org-string" > 'rotating-not-filtered'< / span > , < span class = "org-string" > 'Rz_period'< / span > , 60);
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< / pre >
< / div >
< / div >
< / div >
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< div id = "outline-container-orgc66d5ef" class = "outline-3" >
< h3 id = "orgc66d5ef" > < span class = "section-number-3" > 1.2< / span > Realistic Bending Stiffness Values< / h3 >
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< div class = "outline-text-3" id = "text-1-2" >
< p >
Let’ s compare the ideal case (zero stiffness in rotation and infinite stiffness in translation) with a more realistic case:
< / p >
< ul class = "org-ul" >
< li > \(K_{\theta, \phi} = 15\,[Nm/rad]\) stiffness in flexion< / li >
< li > \(K_{\psi} = 20\,[Nm/rad]\) stiffness in torsion< / li >
< / ul >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > Kf_M = 15< span class = "org-type" > *< / span > ones(6,1);
Kf_F = 15< span class = "org-type" > *< / span > ones(6,1);
Kt_M = 20< span class = "org-type" > *< / span > ones(6,1);
Kt_F = 20< span class = "org-type" > *< / span > ones(6,1);
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< / pre >
< / div >
< p >
The stiffness and damping of the nano-hexapod’ s legs are:
< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > k_opt = 1e5; < span class = "org-comment" > % [N/m]< / span >
c_opt = 2e2; < span class = "org-comment" > % [N/(m/s)]< / span >
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< / pre >
< / div >
< p >
This corresponds to the optimal identified stiffness.
< / p >
< / div >
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< div id = "outline-container-org7f86aa6" class = "outline-4" >
< h4 id = "org7f86aa6" > < span class = "section-number-4" > 1.2.1< / span > Direct Velocity Feedback< / h4 >
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< div class = "outline-text-4" id = "text-1-2-1" >
< p >
We identify the dynamics from actuators force \(\tau_i\) to relative motion sensors \(d\mathcal{L}_i\) with and without considering the flexible joint stiffness.
< / p >
< p >
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The obtained dynamics are shown in Figure < a href = "#orgc127d0f" > 1< / a > .
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It is shown that the adding of stiffness for the flexible joints does increase a little bit the frequencies of the mass suspension modes. It stiffen the structure.
< / p >
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< div id = "orgc127d0f" class = "figure" >
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< p > < img src = "figs/flex_joint_rot_dvf.png" alt = "flex_joint_rot_dvf.png" / >
< / p >
< p > < span class = "figure-number" > Figure 1: < / span > Dynamics from actuators force \(\tau_i\) to relative motion sensors \(d\mathcal{L}_i\) with (blue) and without (red) considering the flexible joint stiffness< / p >
< / div >
< / div >
< / div >
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< div id = "outline-container-orgd763ab8" class = "outline-4" >
< h4 id = "orgd763ab8" > < span class = "section-number-4" > 1.2.2< / span > Primary Plant< / h4 >
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< div class = "outline-text-4" id = "text-1-2-2" >
< p >
Let’ s now identify the dynamics from \(\bm{\tau}^\prime\) to \(\bm{\epsilon}_{\mathcal{X}_n}\) (for the primary controller designed in the frame of the legs).
< / p >
< p >
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The dynamics is compare with and without the joint flexibility in Figure < a href = "#orgbca1f59" > 2< / a > .
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The plant dynamics is not found to be changing significantly.
< / p >
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< div id = "orgbca1f59" class = "figure" >
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< p > < img src = "figs/flex_joints_rot_primary_plant_L.png" alt = "flex_joints_rot_primary_plant_L.png" / >
< / p >
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< p > < span class = "figure-number" > Figure 2: < / span > Dynamics from \(\bm{\tau}^\prime_i\) to \(\bm{\epsilon}_{\mathcal{X}_n,i}\) with perfect joints and with flexible joints< / p >
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< / div >
< / div >
< / div >
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< div id = "outline-container-org34d48fd" class = "outline-4" >
< h4 id = "org34d48fd" > < span class = "section-number-4" > 1.2.3< / span > Conclusion< / h4 >
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< div class = "outline-text-4" id = "text-1-2-3" >
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< div class = "important" id = "org5365e9f" >
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< p >
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Considering realistic flexible joint bending stiffness for the nano-hexapod does not seems to impose any limitation on the DVF control nor on the primary control.
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< / p >
< p >
It only increases a little bit the suspension modes of the sample on top of the nano-hexapod.
< / p >
< / div >
< / div >
< / div >
< / div >
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< div id = "outline-container-org2383b0a" class = "outline-3" >
< h3 id = "org2383b0a" > < span class = "section-number-3" > 1.3< / span > Parametric Study< / h3 >
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< div class = "outline-text-3" id = "text-1-3" >
< p >
We wish now to see what is the impact of the rotation stiffness of the flexible joints on the dynamics.
This will help to determine the requirements on the joint’ s stiffness.
< / p >
< p >
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Let’ s consider the following bending stiffness of the flexible joints:
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< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > Ks = [1, 5, 10, 50, 100]; < span class = "org-comment" > % [Nm/rad]< / span >
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< / pre >
< / div >
< p >
We also consider here a nano-hexapod with the identified optimal actuator stiffness.
< / p >
< / div >
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< div id = "outline-container-org0b2ea81" class = "outline-4" >
< h4 id = "org0b2ea81" > < span class = "section-number-4" > 1.3.1< / span > Direct Velocity Feedback< / h4 >
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< div class = "outline-text-4" id = "text-1-3-1" >
< p >
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The dynamics from the actuators to the relative displacement sensor in each leg is identified and shown in Figure < a href = "#org849b1d6" > 3< / a > .
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< / p >
< p >
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The corresponding Root Locus plot is shown in Figure < a href = "#org311fafc" > 4< / a > .
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< / p >
< p >
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It is shown that the bending stiffness of the flexible joints does indeed change a little the dynamics, but critical damping is stiff achievable with Direct Velocity Feedback.
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< / p >
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< div id = "org849b1d6" class = "figure" >
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< p > < img src = "figs/flex_joints_rot_study_dvf.png" alt = "flex_joints_rot_study_dvf.png" / >
< / p >
< p > < span class = "figure-number" > Figure 3: < / span > Dynamics from \(\tau_i\) to \(d\mathcal{L}_i\) for all the considered Rotation Stiffnesses< / p >
< / div >
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< div id = "org311fafc" class = "figure" >
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< p > < img src = "figs/flex_joints_rot_study_dvf_root_locus.png" alt = "flex_joints_rot_study_dvf_root_locus.png" / >
< / p >
< p > < span class = "figure-number" > Figure 4: < / span > Root Locus for all the considered Rotation Stiffnesses< / p >
< / div >
< / div >
< / div >
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< div id = "outline-container-org4bcbd52" class = "outline-4" >
< h4 id = "org4bcbd52" > < span class = "section-number-4" > 1.3.2< / span > Primary Control< / h4 >
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< div class = "outline-text-4" id = "text-1-3-2" >
< p >
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The dynamics from \(\bm{\tau}^\prime\) to \(\bm{\epsilon}_{\mathcal{X}_n}\) (for the primary controller designed in the frame of the legs) is shown in Figure < a href = "#orgaed64b5" > 5< / a > .
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< / p >
< p >
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It is shown that the bending stiffness of the flexible joints have very little impact on the dynamics.
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< / p >
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< div id = "orgaed64b5" class = "figure" >
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< p > < img src = "figs/flex_joints_rot_study_primary_plant.png" alt = "flex_joints_rot_study_primary_plant.png" / >
< / p >
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< p > < span class = "figure-number" > Figure 5: < / span > Diagonal elements of the transfer function matrix from \(\bm{\tau}^\prime\) to \(\bm{\epsilon}_{\mathcal{X}_n}\) for the considered bending stiffnesses< / p >
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< / div >
< / div >
< / div >
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< div id = "outline-container-orgd481cbd" class = "outline-4" >
< h4 id = "orgd481cbd" > < span class = "section-number-4" > 1.3.3< / span > Conclusion< / h4 >
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< div class = "outline-text-4" id = "text-1-3-3" >
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< div class = "important" id = "org98dc84f" >
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< p >
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The bending stiffness of the flexible joint does not significantly change the dynamics.
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< / p >
< / div >
< / div >
< / div >
< / div >
< / div >
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< div id = "outline-container-org122af58" class = "outline-2" >
< h2 id = "org122af58" > < span class = "section-number-2" > 2< / span > Axial Stiffness< / h2 >
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< div class = "outline-text-2" id = "text-2" >
< p >
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< a id = "org7789cf6" > < / a >
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< / p >
< p >
Let’ s know consider a flexibility in translation of the flexible joint, in the axis of the legs.
< / p >
< / div >
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< div id = "outline-container-orgbd421fd" class = "outline-3" >
< h3 id = "orgbd421fd" > < span class = "section-number-3" > 2.1< / span > Realistic Translation Stiffness Values< / h3 >
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< div class = "outline-text-3" id = "text-2-1" >
< p >
We choose realistic values of the axial stiffness of the joints:
\[ K_a = 60\,[N/\mu m] \]
< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > Ka_F = 60e6< span class = "org-type" > *< / span > ones(6,1); < span class = "org-comment" > % [N/m]< / span >
Ka_M = 60e6< span class = "org-type" > *< / span > ones(6,1); < span class = "org-comment" > % [N/m]< / span >
Ca_F = 1< span class = "org-type" > *< / span > ones(6,1); < span class = "org-comment" > % [N/(m/s)]< / span >
Ca_M = 1< span class = "org-type" > *< / span > ones(6,1); < span class = "org-comment" > % [N/(m/s)]< / span >
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< / pre >
< / div >
< / div >
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< div id = "outline-container-org7e915de" class = "outline-4" >
< h4 id = "org7e915de" > < span class = "section-number-4" > 2.1.1< / span > Initialization< / h4 >
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< div class = "outline-text-4" id = "text-2-1-1" >
< p >
Let’ s initialize all the stages with default parameters.
< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > initializeGround();
initializeGranite();
initializeTy();
initializeRy();
initializeRz();
initializeMicroHexapod();
initializeAxisc();
initializeMirror();
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< / pre >
< / div >
< p >
Let’ s consider the heaviest mass which should we the most problematic with it comes to the flexible joints.
< / p >
< div class = "org-src-container" >
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< pre class = "src src-matlab" > initializeSample(< span class = "org-string" > 'mass'< / span > , 50, < span class = "org-string" > 'freq'< / span > , 200< span class = "org-type" > *< / span > ones(6,1));
initializeReferences(< span class = "org-string" > 'Rz_type'< / span > , < span class = "org-string" > 'rotating-not-filtered'< / span > , < span class = "org-string" > 'Rz_period'< / span > , 60);
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< / pre >
< / div >
< / div >
< / div >
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< div id = "outline-container-org484b32d" class = "outline-4" >
< h4 id = "org484b32d" > < span class = "section-number-4" > 2.1.2< / span > Direct Velocity Feedback< / h4 >
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< p >
The dynamics from actuators force \(\tau_i\) to relative motion sensors \(d\mathcal{L}_i\) with and without considering the flexible joint stiffness are identified.
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< p >
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The obtained dynamics are shown in Figure < a href = "#org90e79ad" > 6< / a > .
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< div id = "org90e79ad" class = "figure" >
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< p > < img src = "figs/flex_joint_trans_dvf.png" alt = "flex_joint_trans_dvf.png" / >
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< p > < span class = "figure-number" > Figure 6: < / span > Dynamics from actuators force \(\tau_i\) to relative motion sensors \(d\mathcal{L}_i\) with (blue) and without (red) considering the flexible joint axis stiffness< / p >
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< h4 id = "org4c02123" > < span class = "section-number-4" > 2.1.3< / span > Primary Plant< / h4 >
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< pre class = "src src-matlab" > Kdvf = 5e3< span class = "org-type" > *< / span > s< span class = "org-type" > /< / span > (1< span class = "org-type" > +< / span > s< span class = "org-type" > /< / span > 2< span class = "org-type" > /< / span > < span class = "org-constant" > pi< / span > < span class = "org-type" > /< / span > 1e3)< span class = "org-type" > *< / span > eye(6);
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< / pre >
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< p >
Let’ s now identify the dynamics from \(\bm{\tau}^\prime\) to \(\bm{\epsilon}_{\mathcal{X}_n}\) (for the primary controller designed in the frame of the legs).
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< p >
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The dynamics is compare with and without the joint flexibility in Figure < a href = "#org98bb072" > 7< / a > .
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< div id = "org98bb072" class = "figure" >
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< p > < img src = "figs/flex_joints_trans_primary_plant_L.png" alt = "flex_joints_trans_primary_plant_L.png" / >
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< p > < span class = "figure-number" > Figure 7: < / span > Dynamics from \(\bm{\tau}^\prime_i\) to \(\bm{\epsilon}_{\mathcal{X}_n,i}\) with infinite axis stiffnes (solid) and with realistic axial stiffness (dashed)< / p >
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< div id = "outline-container-org8aa50f5" class = "outline-4" >
< h4 id = "org8aa50f5" > < span class = "section-number-4" > 2.1.4< / span > Conclusion< / h4 >
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< div class = "outline-text-4" id = "text-2-1-4" >
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< div class = "important" id = "org2e8394a" >
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< p >
For the realistic value of the flexible joint axial stiffness, the dynamics is not much impact, and this should not be a problem for control.
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< h3 id = "orge0a9c34" > < span class = "section-number-3" > 2.2< / span > Parametric study< / h3 >
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< div class = "outline-text-3" id = "text-2-2" >
< p >
We wish now to see what is the impact of the < b > axial< / b > stiffness of the flexible joints on the dynamics.
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< p >
Let’ s consider the following values for the axial stiffness:
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< pre class = "src src-matlab" > Kas = [1e4, 1e5, 1e6, 1e7, 1e8, 1e9]; < span class = "org-comment" > % [N/m]< / span >
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< p >
We also consider here a nano-hexapod with the identified optimal actuator stiffness (\(k = 10^5\,[N/m]\)).
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< h4 id = "org564cc95" > < span class = "section-number-4" > 2.2.1< / span > Direct Velocity Feedback< / h4 >
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< div class = "outline-text-4" id = "text-2-2-1" >
< p >
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The dynamics from the actuators to the relative displacement sensor in each leg is identified and shown in Figure < a href = "#orgeed898e" > 8< / a > .
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< / p >
< p >
It is shown that the axial stiffness of the flexible joints does have a huge impact on the dynamics.
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< p >
If the axial stiffness of the flexible joints is \(K_a > 10^7\,[N/m]\) (here \(100\) times higher than the actuator stiffness), then the change of dynamics stays reasonably small.
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< p >
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This is more clear by looking at the root locus (Figures < a href = "#org399589b" > 9< / a > and < a href = "#org5154002" > 10< / a > ).
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It can be seen that very little active damping can be achieve for axial stiffnesses below \(10^7\,[N/m]\).
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< div id = "orgeed898e" class = "figure" >
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< p > < img src = "figs/flex_joints_trans_study_dvf.png" alt = "flex_joints_trans_study_dvf.png" / >
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< p > < span class = "figure-number" > Figure 8: < / span > Dynamics from \(\tau_i\) to \(d\mathcal{L}_i\) for all the considered axis Stiffnesses< / p >
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< div id = "org399589b" class = "figure" >
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< p > < img src = "figs/flex_joints_trans_study_dvf_root_locus.png" alt = "flex_joints_trans_study_dvf_root_locus.png" / >
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< p > < span class = "figure-number" > Figure 9: < / span > Root Locus for all the considered axial Stiffnesses< / p >
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< div id = "org5154002" class = "figure" >
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< p > < img src = "figs/flex_joints_trans_study_root_locus_unzoom.png" alt = "flex_joints_trans_study_root_locus_unzoom.png" / >
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< p > < span class = "figure-number" > Figure 10: < / span > Root Locus (unzoom) for all the considered axial Stiffnesses< / p >
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< div id = "outline-container-orgc1721b8" class = "outline-4" >
< h4 id = "orgc1721b8" > < span class = "section-number-4" > 2.2.2< / span > Primary Control< / h4 >
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< div class = "outline-text-4" id = "text-2-2-2" >
< p >
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The dynamics from \(\bm{\tau}^\prime\) to \(\bm{\epsilon}_{\mathcal{X}_n}\) (for the primary controller designed in the frame of the legs) is shown in Figure < a href = "#orgcab6267" > 11< / a > .
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< / p >
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< div id = "orgcab6267" class = "figure" >
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< p > < img src = "figs/flex_joints_trans_study_primary_plant.png" alt = "flex_joints_trans_study_primary_plant.png" / >
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< p > < span class = "figure-number" > Figure 11: < / span > Diagonal elements of the transfer function matrix from \(\bm{\tau}^\prime\) to \(\bm{\epsilon}_{\mathcal{X}_n}\) for the considered axial stiffnesses< / p >
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< h3 id = "org13f48c9" > < span class = "section-number-3" > 2.3< / span > Conclusion< / h3 >
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< div class = "outline-text-3" id = "text-2-3" >
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< div class = "important" id = "org4a497ad" >
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< p >
The axial stiffness of the flexible joints should be maximized.
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< p >
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For the considered actuator stiffness \(k = 10^5\,[N/m]\), the axial stiffness of the flexible joints should ideally be above \(10^7\,[N/m]\).
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< / p >
< p >
This is a reasonable stiffness value for such joints.
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< p >
We may interpolate the results and say that the axial joint stiffness should be 100 times higher than the actuator stiffness, but this should be confirmed with further analysis.
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< h2 id = "org5519f74" > < span class = "section-number-2" > 3< / span > Conclusion< / h2 >
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< p >
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< a id = "org8e0b118" > < / a >
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< div class = "important" id = "org3aeae4e" >
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< p >
In this study we considered the bending, torsional and axial stiffnesses of the flexible joints used for the nano-hexapod.
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< p >
The bending and torsional stiffnesses somehow adds a parasitic stiffness in parallel with the legs.
It is not found to be much problematic for the considered control architecture (it is however, if Integral Force Feedback is to be used).
As a consequence of the added stiffness, it could increase a little bit the required actuator force.
< / p >
< p >
The axial stiffness of the flexible joints can be very problematic for control.
Small values of the axial stiffness are shown to limit the achievable damping with Direct Velocity Feedback.
The axial stiffness should therefore be maximized and taken into account in the model of the nano-hexapod.
< / p >
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< p >
For the identified optimal actuator stiffness \(k = 10^5\,[N/m]\), the flexible joint should have the following stiffness properties:
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< ul class = "org-ul" >
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< li > Axial Stiffness: \(K_a > 10^7\,[N/m]\)< / li >
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< li > Bending Stiffness: \(K_b < 50 \ , [ Nm / rad ] \ ) < / li >
< li > Torsion Stiffness: \(K_t < 50 \ , [ N m / rad ] \ ) < / li >
< / ul >
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< p >
As there is generally a trade-off between bending stiffness and axial stiffness, it should be highlighted that the < b > axial< / b > stiffness is the most important property of the flexible joints.
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< h2 id = "org358d063" > < span class = "section-number-2" > 4< / span > Designed Flexible Joints< / h2 >
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< h3 id = "org1148778" > < span class = "section-number-3" > 4.1< / span > Initialization< / h3 >
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Let’ s initialize all the stages with default parameters.
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< pre class = "src src-matlab" > initializeGround();
initializeGranite();
initializeTy();
initializeRy();
initializeRz();
initializeMicroHexapod();
initializeAxisc(< span class = "org-string" > 'type'< / span > , < span class = "org-string" > 'none'< / span > );
initializeMirror(< span class = "org-string" > 'type'< / span > , < span class = "org-string" > 'none'< / span > );
initializeMirror();
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Let’ s consider the heaviest mass which should we the most problematic with it comes to the flexible joints.
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< pre class = "src src-matlab" > initializeSample(< span class = "org-string" > 'mass'< / span > , 50, < span class = "org-string" > 'freq'< / span > , 200< span class = "org-type" > *< / span > ones(6,1));
initializeReferences(< span class = "org-string" > 'Rz_type'< / span > , < span class = "org-string" > 'rotating-not-filtered'< / span > , < span class = "org-string" > 'Rz_period'< / span > , 60);
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< pre class = "src src-matlab" > flex_joint = load(< span class = "org-string" > './mat/flexor_025.mat'< / span > , < span class = "org-string" > 'int_xyz'< / span > , < span class = "org-string" > 'int_i'< / span > , < span class = "org-string" > 'n_xyz'< / span > , < span class = "org-string" > 'n_i'< / span > , < span class = "org-string" > 'nodes'< / span > , < span class = "org-string" > 'M'< / span > , < span class = "org-string" > 'K'< / span > );
apa = load(< span class = "org-string" > './mat/APA300ML_simplified_model.mat'< / span > );
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< pre class = "src src-matlab" > initializeNanoHexapod(< span class = "org-string" > 'actuator'< / span > , < span class = "org-string" > 'amplified'< / span > , ...
< span class = "org-string" > 'ke'< / span > , apa.ke, < span class = "org-string" > 'ka'< / span > , apa.ka, < span class = "org-string" > 'k1'< / span > , apa.k1, < span class = "org-string" > 'c1'< / span > , apa.c1, < span class = "org-string" > 'F_gain'< / span > , apa.F_gain, ...
< span class = "org-string" > 'type_M'< / span > , < span class = "org-string" > 'spherical_3dof'< / span > , ...
< span class = "org-string" > 'Kr_M'< / span > , flex_joint.K(1,1)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'Ka_M'< / span > , flex_joint.K(3,3)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'Kf_M'< / span > , flex_joint.K(4,4)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'Kt_M'< / span > , flex_joint.K(6,6)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'type_F'< / span > , < span class = "org-string" > 'spherical_3dof'< / span > , ...
< span class = "org-string" > 'Kr_F'< / span > , flex_joint.K(1,1)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'Ka_F'< / span > , flex_joint.K(3,3)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'Kf_F'< / span > , flex_joint.K(4,4)< span class = "org-type" > *< / span > ones(6,1), ...
< span class = "org-string" > 'Kt_F'< / span > , flex_joint.K(6,6)< span class = "org-type" > *< / span > ones(6,1));
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< pre class = "src src-matlab" > initializeNanoHexapod();
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< h3 id = "orgd889755" > < span class = "section-number-3" > 4.2< / span > Direct Velocity Feedback< / h3 >
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< h3 id = "org12972b2" > < span class = "section-number-3" > 4.3< / span > Integral Force Feedback< / h3 >
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< div id = "postamble" class = "status" >
< p class = "author" > Author: Dehaeze Thomas< / p >
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< p class = "date" > Created: 2021-02-20 sam. 23:09< / p >
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