Add figs about cubic architecture, flexible joints
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figs/3d-cubic-stewart-aligned.png
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figs/dvf_root_locus_ws.png
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figs/iff_root_locus_ws.png
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figs/mobility_translations_null_rotation.png
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figs/preumont07_flexible_joints.png
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figs/root_locus_dvf_rot_stiffness.png
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figs/yang19_flexible_joints.png
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index.html
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index.org
@ -604,6 +604,7 @@ The ASD contains any peaks starting from 1Hz showing the large spectral content
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#+begin_important
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#+begin_important
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A smoother motion for the translation stage (such as a sinus motion, of a filtered triangular signal) could help reducing much of the vibrations.
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A smoother motion for the translation stage (such as a sinus motion, of a filtered triangular signal) could help reducing much of the vibrations.
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The goal is to inject no motion outside the control bandwidth.
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We should also note that away from the rapid change of velocity, the sample's vibrations are much reduced.
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We should also note that away from the rapid change of velocity, the sample's vibrations are much reduced.
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Thus, if the detector is only used in between the triangular peaks, the vibrations are expected to be much lower than those estimated.
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Thus, if the detector is only used in between the triangular peaks, the vibrations are expected to be much lower than those estimated.
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@ -758,8 +759,9 @@ The results of this simulation will be compared to simulations using the NASS in
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An 3D animation of the simulation is shown in Figure [[fig:open_loop_sim]].
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An 3D animation of the simulation is shown in Figure [[fig:open_loop_sim]].
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A zoom in the micro-meter ranger on the sample's location is shown in Figure [[fig:open_loop_sim_zoom]] with two frames:
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A zoom in the micro-meter ranger on the sample's location is shown in Figure [[fig:open_loop_sim_zoom]] with two frames:
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- a non-rotating frame corresponding to the wanted position of the sample.
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- a non-rotating frame corresponding to the focusing point of the X-ray.
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Note that this frame is moving with the granite.
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It does in that case correspond to the wanted position of the sample.
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Note that this frame is moving with the granite as the nano-focusing optics are fixed to the granite.
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- a rotating frame that corresponds to the actual pose of the sample
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- a rotating frame that corresponds to the actual pose of the sample
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The motion of the sample follows the wanted motion but with vibrations in the micro-meter range as was expected.
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The motion of the sample follows the wanted motion but with vibrations in the micro-meter range as was expected.
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@ -803,17 +805,20 @@ In the next sections, it will allows to optimally design the nano-hexapod, to de
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<<sec:nano_hexapod_design>>
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<<sec:nano_hexapod_design>>
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** Introduction :ignore:
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** Introduction :ignore:
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As explain before, the nano-hexapod properties (mass, stiffness, architecture, ...) will influence:
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As explain before, the nano-hexapod properties (mass, stiffness, legs' orientation, ...) will influence:
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- the effect of disturbances $G_d$ (important for the rejection of disturbances)
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- the effect of disturbances $G_d$ (important for the rejection of disturbances)
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- the plant dynamics $G$ (important for the control robustness properties)
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- the plant dynamics $G$ (important for the control robustness properties)
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Thus, we here wish to find the optimal nano-hexapod properties such that:
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Thus, we here wish to find the optimal nano-hexapod properties such that:
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- the effect of disturbances is minimized (Section [[sec:optimal_stiff_dist]])
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- the effect of disturbances is minimized (Section [[sec:optimal_stiff_dist]])
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- the plant uncertainty due to a change of payload mass and experimental conditions is minimized (Section [[sec:optimal_stiff_plant]])
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- the plant uncertainty due to a change of payload mass and experimental conditions is minimized (Section [[sec:optimal_stiff_plant]])
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- the plant has nice dynamical properties for control (Section [[sec:nano_hexapod_architecture]])
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The study presented here only consider changes in the nano-hexapod *stiffness* for two reasons:
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In this study, the effect of the nano-hexapod's mass characteristics is not taken into account because:
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- the nano-hexapod mass cannot be change too much, and will anyway be negligible compare to the metrology reflector and the payload masses
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1. it cannot be changed a lot
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- the choice of the nano-hexapod architecture (e.g. orientations of the actuators and implementation of sensors) will be further studied in accord with the control architecture
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2. it is quite negligible compare the to metrology reflector and the payload's masses that is fixed to nano-hexapod's top platform
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Also, the effect of the nano-hexapod's damping properties will be studied when applying active damping techniques.
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** Optimal Stiffness to reduce the effect of disturbances
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** Optimal Stiffness to reduce the effect of disturbances
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<<sec:optimal_stiff_dist>>
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<<sec:optimal_stiff_dist>>
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@ -1043,6 +1048,127 @@ This show how the dynamics evolves with the stiffness and how different effects
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In such case, the main limitation will be heavy samples with small stiffnesses.
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In such case, the main limitation will be heavy samples with small stiffnesses.
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#+end_important
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#+end_important
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** Nano-Hexapod Architecture
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<<sec:nano_hexapod_architecture>>
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*** Introduction :ignore:
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*** Kinematic Analysis - Jacobian Matrix
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:PROPERTIES:
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:UNNUMBERED: t
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:END:
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The kinematic analysis of a parallel manipulator is well described in cite:taghirad13_paral:
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#+begin_quote
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Kinematic analysis refers to the study of the geometry of motion of a robot, without considering the forces an torques that cause the motion.
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In this analysis, the relation between the geometrical parameters of the manipulator with the final motion of the moving platform is derived and analyzed.
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#+end_quote
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From cite:taghirad13_paral:
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#+begin_quote
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The Jacobian matrix not only reveals the *relation between the joint variable velocities of a parallel manipulator to the moving platform linear and angular velocities*, it also constructs the transformation needed to find the *actuator forces from the forces and moments acting on the moving platform*.
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#+end_quote
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The Jacobian matrix $\bm{\mathcal{J}}$ can be computed form the orientation of the legs and the position of the flexible joints.
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If we note:
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- $\delta\bm{\mathcal{L}} = [ \delta l_1, \delta l_2, \delta l_3, \delta l_4, \delta l_5, \delta l_6 ]^T$: the vector of small legs' displacements
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- $\delta \bm{\mathcal{X}} = [\delta x, \delta y, \delta z, \delta \theta_x, \delta \theta_y, \delta \theta_z ]^T$: the vector of small mobile platform displacements
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The Jacobian matrix links the two vectors:
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\begin{align*}
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\delta\bm{\mathcal{L}} &= \bm{J} \delta\bm{\mathcal{X}} \\
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\delta\bm{\mathcal{X}} &= \bm{J}^{-1} \delta\bm{\mathcal{L}}
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\end{align*}
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If we note:
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- $\bm{\tau} = [\tau_1, \tau_2, \cdots, \tau_6]^T$: vector of actuator forces applied in each strut
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- $\bm{\mathcal{F}} = [\bm{f}, \bm{n}]^T$: external force/torque action on the mobile platform
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\begin{equation*}
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\bm{\mathcal{F}} = \bm{J}^T \bm{\tau}
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\end{equation*}
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\begin{equation*}
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\bm{\mathcal{F}} = \bm{K} \delta \bm{\mathcal{X}}
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\end{equation*}
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\begin{equation*}
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\bm{K} = \bm{J}^T \mathcal{K} \bm{J}
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\end{equation*}
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\begin{equation*}
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\bm{C} = \bm{K}^{-1} = (\bm{J}^T \mathcal{K} \bm{J})^{-1}
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\end{equation*}
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Kinematic Study https://tdehaeze.github.io/stewart-simscape/kinematic-study.html
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Mobility can be estimated from the architecture of the Stewart platform and the leg's stroke.
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Stiffness properties is estimated from the architecture and leg's stiffness
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*** Kinematic Analysis - Mobility
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:PROPERTIES:
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:UNNUMBERED: t
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:END:
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#+name: fig:mobility_translations_null_rotation
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#+caption: Figure caption
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[[file:figs/mobility_translations_null_rotation.png]]
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*** Kinematic Study
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||||||
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:PROPERTIES:
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||||||
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:UNNUMBERED: t
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||||||
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:END:
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||||||
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*** Flexible Joints
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:PROPERTIES:
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:UNNUMBERED: t
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:END:
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Active Damping Study https://tdehaeze.github.io/stewart-simscape/control-active-damping.html
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Flexible Joint stiffness => not problematic for the chosen active damping technique
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#+name: tab:yang19_stiffness_flexible_joints
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#+caption: Stiffness of flexible joints
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| $k_{\theta u},\ k_{\psi u}$ | $72 Nm/rad$ |
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| $k_{\theta s}$ | $51 Nm/rad$ |
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| $k_{\psi s}$ | $62 Nm/rad$ |
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| $k_{\gamma s}$ | $64 Nm/rad$ |
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#+name: fig:preumont07_flexible_joints
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#+caption: Figure caption cite:preumont07_six_axis_singl_stage_activ
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[[file:figs/preumont07_flexible_joints.png]]
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|
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#+name: fig:yang19_flexible_joints
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#+caption: Figure caption
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[[file:figs/yang19_flexible_joints.png]]
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*** Cubic Architecture
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:PROPERTIES:
|
||||||
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:UNNUMBERED: t
|
||||||
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:END:
|
||||||
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Study of cubic architecture https://tdehaeze.github.io/stewart-simscape/cubic-configuration.html
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Has some advantages such as uniform stiffness and uniform mobility.
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It can have very nice properties in specific conditions that will not be the case for this application.
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The cubic configuration also puts much restriction on the position and orientation of each leg.
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This configuration is such not recommended.
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#+name: fig:3d-cubic-stewart-aligned
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||||||
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#+caption: Figure caption
|
||||||
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[[file:figs/3d-cubic-stewart-aligned.png]]
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||||||
** Conclusion
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** Conclusion
|
||||||
#+begin_important
|
#+begin_important
|
||||||
In Section [[sec:optimal_stiff_dist]], it has been concluded that a nano-hexapod stiffness below $10^5-10^6\,[N/m]$ helps reducing the high frequency vibrations induced by all sources of disturbances considered.
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In Section [[sec:optimal_stiff_dist]], it has been concluded that a nano-hexapod stiffness below $10^5-10^6\,[N/m]$ helps reducing the high frequency vibrations induced by all sources of disturbances considered.
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@ -1102,19 +1228,39 @@ The HAC-LAC architecture thus consisted of two cascade controllers:
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** Active Damping and Sensors to be included in the nano-hexapod
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** Active Damping and Sensors to be included in the nano-hexapod
|
||||||
<<sec:lac_control>>
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<<sec:lac_control>>
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||||||
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|
||||||
Active Damping can help:
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*** Introduction :ignore:
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||||||
- by reducing the effect of disturbances close to the resonance of the system
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- by making the plant dynamics simpler to control for the High Authority Controller
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Depending on the chosen active damping technique, either force sensors, relative motion sensors or inertial sensors should be included in each of the nano-hexapod's legs.
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Depending on the chosen active damping technique, either force sensors, relative motion sensors or inertial sensors should be included in each of the nano-hexapod's legs.
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Because of the rotation of the hexapod,
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A separate study (accessible [[https://tdehaeze.github.io/rotating-frame/index.html][here]]) about the use of all three sensors types have been done, the conclusions are:
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A separate study (accessible [[https://tdehaeze.github.io/rotating-frame/index.html][here]]) about the use of all three sensors types have been done, the conclusions are:
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||||||
- the use of force sensors is to be avoided as it could introduce instability in the system due to the nano-hexapod's rotation
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- the use of force sensors is to be avoided as it could introduce instability in the system due to the nano-hexapod's rotation
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||||||
- the use of inertial sensor should not be used as it would tends to decouple the motion of the sample from the motion of the granite (which is not wanted).
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- the use of inertial sensor should not be used as it would tends to decouple the motion of the sample from the motion of the granite (which is not wanted).
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It would also be difficult to apply in a robust way due to the non-collocation with the actuators
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It would also be difficult to apply in a robust way due to the non-collocation with the actuators
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||||||
- relative motion sensors can be used to damped the nano-hexapod's modes in a robust way but may increase the sensibility to stages vibrations
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- relative motion sensors can be used to damped the nano-hexapod's modes in a robust way but may increase the sensibility to stages vibrations
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||||||
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||||||
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*** Effect of the Spindle's Rotation
|
||||||
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:PROPERTIES:
|
||||||
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:UNNUMBERED: t
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:END:
|
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#+name: fig:dvf_root_locus_ws
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#+caption: Figure caption
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||||||
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[[file:figs/dvf_root_locus_ws.png]]
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#+name: fig:iff_root_locus_ws
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||||||
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#+caption: Figure caption
|
||||||
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[[file:figs/iff_root_locus_ws.png]]
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||||||
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|
||||||
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*** Relative Direct Velocity Feedback Architecture
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||||||
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:PROPERTIES:
|
||||||
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:UNNUMBERED: t
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:END:
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||||||
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|
||||||
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Active Damping can help:
|
||||||
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- by reducing the effect of disturbances close to the resonance of the system
|
||||||
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- by making the plant dynamics simpler to control for the High Authority Controller
|
||||||
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|
||||||
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||||||
*Relative motion sensors* are then included in each of the nano-hexapod's leg and a decentralized direct velocity feedback control architecture is applied (Figure [[fig:control_architecture_dvf]]).
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*Relative motion sensors* are then included in each of the nano-hexapod's leg and a decentralized direct velocity feedback control architecture is applied (Figure [[fig:control_architecture_dvf]]).
|
||||||
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|
||||||
@ -1135,6 +1281,10 @@ The force applied in each leg being proportional to the relative velocity of the
|
|||||||
The DVF gain is here chosen in such a way that the suspension modes of the nano-hexapod are critically damped whatever the sample mass.
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The DVF gain is here chosen in such a way that the suspension modes of the nano-hexapod are critically damped whatever the sample mass.
|
||||||
This may not be the optimal choice as will be further explained.
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This may not be the optimal choice as will be further explained.
|
||||||
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|
||||||
|
*** Effect of Active Damping on the Primary Plant Dynamics
|
||||||
|
:PROPERTIES:
|
||||||
|
:UNNUMBERED: t
|
||||||
|
:END:
|
||||||
|
|
||||||
The plant dynamics before (solid curves) and after (dashed curves) the Low Authority Control implementation are compared in Figure [[fig:opt_stiff_primary_plant_damped_L]].
|
The plant dynamics before (solid curves) and after (dashed curves) the Low Authority Control implementation are compared in Figure [[fig:opt_stiff_primary_plant_damped_L]].
|
||||||
It is clear that the use of the DVF reduces the dynamical spread of the plant dynamics between 5Hz up too 100Hz.
|
It is clear that the use of the DVF reduces the dynamical spread of the plant dynamics between 5Hz up too 100Hz.
|
||||||
@ -1144,6 +1294,11 @@ This will make the primary controller more robust and easier to develop.
|
|||||||
#+caption: Primary plant in the space of the legs with (dashed) and without (solid) Direct Velocity Feedback
|
#+caption: Primary plant in the space of the legs with (dashed) and without (solid) Direct Velocity Feedback
|
||||||
[[file:figs/opt_stiff_primary_plant_damped_L.png]]
|
[[file:figs/opt_stiff_primary_plant_damped_L.png]]
|
||||||
|
|
||||||
|
*** Effect of Active Damping on the Sensibility to Disturbances
|
||||||
|
:PROPERTIES:
|
||||||
|
:UNNUMBERED: t
|
||||||
|
:END:
|
||||||
|
|
||||||
The change of sensibility to disturbances with the use of DVF is shown in Figure [[fig:opt_stiff_sensibility_dist_dvf]].
|
The change of sensibility to disturbances with the use of DVF is shown in Figure [[fig:opt_stiff_sensibility_dist_dvf]].
|
||||||
It is shown that the DVF control lowers the sensibility to disturbances in the vicinity of the nano-hexapod resonance but increases the sensibility at higher frequencies.
|
It is shown that the DVF control lowers the sensibility to disturbances in the vicinity of the nano-hexapod resonance but increases the sensibility at higher frequencies.
|
||||||
|
|
||||||
@ -1250,14 +1405,24 @@ An animation of the experiment is shown in Figure [[fig:closed_loop_sim_zoom]] a
|
|||||||
[[file:figs/closed_loop_sim_zoom.gif]]
|
[[file:figs/closed_loop_sim_zoom.gif]]
|
||||||
|
|
||||||
** Simulation of More Complex Experiments
|
** Simulation of More Complex Experiments
|
||||||
|
*** Introduction :ignore:
|
||||||
|
|
||||||
|
*** Micro-Hexapod offset
|
||||||
|
:PROPERTIES:
|
||||||
|
:UNNUMBERED: t
|
||||||
|
:END:
|
||||||
|
|
||||||
#+name: fig:tomography_dh_offset
|
#+name: fig:tomography_dh_offset
|
||||||
#+caption: Figure caption
|
#+caption: Top View of a tomography experiment with a 10mm offset imposed by the micro-hexapod
|
||||||
[[file:figs/tomography_dh_offset.gif]]
|
[[file:figs/tomography_dh_offset.gif]]
|
||||||
|
|
||||||
|
*** Simultaneous Translation Scans
|
||||||
|
:PROPERTIES:
|
||||||
|
:UNNUMBERED: t
|
||||||
|
:END:
|
||||||
|
|
||||||
#+name: fig:ty_scans
|
#+name: fig:ty_scans
|
||||||
#+caption: Figure caption
|
#+caption: Top View of a tomography experiment combined with translation scans
|
||||||
[[file:figs/ty_scans.gif]]
|
[[file:figs/ty_scans.gif]]
|
||||||
|
|
||||||
** Conclusion
|
** Conclusion
|
||||||
@ -1281,6 +1446,8 @@ A more complete study of the control of the NASS is performed [[https://tdehaeze
|
|||||||
* General Conclusion and Further notes
|
* General Conclusion and Further notes
|
||||||
<<sec:conclusion_and_further_notes>>
|
<<sec:conclusion_and_further_notes>>
|
||||||
|
|
||||||
|
** Nano-Hexapod Specifications
|
||||||
|
|
||||||
** General Conclusion
|
** General Conclusion
|
||||||
|
|
||||||
|
|
||||||
@ -1291,8 +1458,10 @@ This should not be significant.
|
|||||||
|
|
||||||
** Further Work
|
** Further Work
|
||||||
|
|
||||||
|
** Cable Forces
|
||||||
|
|
||||||
** Using soft mounts for the
|
|
||||||
|
** Using soft mounts for the Granite
|
||||||
<<sec:soft_granite>>
|
<<sec:soft_granite>>
|
||||||
|
|
||||||
#+name: fig:opt_stiff_soft_granite_Dw
|
#+name: fig:opt_stiff_soft_granite_Dw
|
||||||
|
37
ref.bib
@ -3,7 +3,6 @@
|
|||||||
title = {The Design of High Performance Mechatronics - 2nd Revised Edition},
|
title = {The Design of High Performance Mechatronics - 2nd Revised Edition},
|
||||||
year = {2014},
|
year = {2014},
|
||||||
publisher = {Ios Press},
|
publisher = {Ios Press},
|
||||||
tags = {favorite},
|
|
||||||
}
|
}
|
||||||
|
|
||||||
@article{oomen18_advan_motion_contr_precis_mechat,
|
@article{oomen18_advan_motion_contr_precis_mechat,
|
||||||
@ -16,7 +15,6 @@
|
|||||||
year = {2018},
|
year = {2018},
|
||||||
doi = {10.1541/ieejjia.7.127},
|
doi = {10.1541/ieejjia.7.127},
|
||||||
url = {https://doi.org/10.1541/ieejjia.7.127},
|
url = {https://doi.org/10.1541/ieejjia.7.127},
|
||||||
tags = {favorite},
|
|
||||||
}
|
}
|
||||||
|
|
||||||
@book{preumont18_vibrat_contr_activ_struc_fourt_edition,
|
@book{preumont18_vibrat_contr_activ_struc_fourt_edition,
|
||||||
@ -28,5 +26,40 @@
|
|||||||
doi = {10.1007/978-3-319-72296-2},
|
doi = {10.1007/978-3-319-72296-2},
|
||||||
pages = {nil},
|
pages = {nil},
|
||||||
series = {Solid Mechanics and Its Applications},
|
series = {Solid Mechanics and Its Applications},
|
||||||
|
}
|
||||||
|
|
||||||
|
@book{taghirad13_paral,
|
||||||
|
author = {Taghirad, Hamid},
|
||||||
|
title = {Parallel robots : mechanics and control},
|
||||||
|
year = {2013},
|
||||||
|
publisher = {CRC Press},
|
||||||
|
address = {Boca Raton, FL},
|
||||||
|
isbn = {9781466555778},
|
||||||
tags = {favorite, parallel robot},
|
tags = {favorite, parallel robot},
|
||||||
}
|
}
|
||||||
|
|
||||||
|
@article{yang19_dynam_model_decoup_contr_flexib,
|
||||||
|
author = {Yang, XiaoLong and Wu, HongTao and Chen, Bai and Kang, ShengZheng and Cheng, ShiLi},
|
||||||
|
title = {Dynamic Modeling and Decoupled Control of a Flexible Stewart Platform for Vibration Isolation},
|
||||||
|
journal = {Journal of Sound and Vibration},
|
||||||
|
volume = {439},
|
||||||
|
pages = {398-412},
|
||||||
|
year = {2019},
|
||||||
|
doi = {10.1016/j.jsv.2018.10.007},
|
||||||
|
url = {https://doi.org/10.1016/j.jsv.2018.10.007},
|
||||||
|
issn = {0022-460X},
|
||||||
|
month = {Jan},
|
||||||
|
publisher = {Elsevier BV},
|
||||||
|
}
|
||||||
|
|
||||||
|
@article{preumont07_six_axis_singl_stage_activ,
|
||||||
|
author = {A. Preumont and M. Horodinca and I. Romanescu and B. de Marneffe and M. Avraam and A. Deraemaeker and F. Bossens and A. Abu Hanieh},
|
||||||
|
title = {A Six-Axis Single-Stage Active Vibration Isolator Based on Stewart Platform},
|
||||||
|
journal = {Journal of Sound and Vibration},
|
||||||
|
volume = {300},
|
||||||
|
number = {3-5},
|
||||||
|
pages = {644-661},
|
||||||
|
year = {2007},
|
||||||
|
doi = {10.1016/j.jsv.2006.07.050},
|
||||||
|
url = {https://doi.org/10.1016/j.jsv.2006.07.050},
|
||||||
|
}
|
||||||
|