Add figs about cubic architecture, flexible joints
							
								
								
									
										
											BIN
										
									
								
								figs/3d-cubic-stewart-aligned.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 22 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/dvf_root_locus_ws.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 43 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/iff_root_locus_ws.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 53 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/mobility_translations_null_rotation.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 183 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/preumont07_flexible_joints.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 48 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/root_locus_dvf_rot_stiffness.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 71 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/root_locus_iff_rot_stiffness.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 88 KiB  | 
							
								
								
									
										
											BIN
										
									
								
								figs/yang19_flexible_joints.png
									
									
									
									
									
										Normal file
									
								
							
							
						
						| 
		 After Width: | Height: | Size: 84 KiB  | 
							
								
								
									
										1054
									
								
								index.html
									
									
									
									
									
								
							
							
						
						
							
								
								
									
										197
									
								
								index.org
									
									
									
									
									
								
							
							
						
						@@ -604,6 +604,7 @@ The ASD contains any peaks starting from 1Hz showing the large spectral content
 | 
			
		||||
 | 
			
		||||
#+begin_important
 | 
			
		||||
  A smoother motion for the translation stage (such as a sinus motion, of a filtered triangular signal) could help reducing much of the vibrations.
 | 
			
		||||
  The goal is to inject no motion outside the control bandwidth.
 | 
			
		||||
 | 
			
		||||
  We should also note that away from the rapid change of velocity, the sample's vibrations are much reduced.
 | 
			
		||||
  Thus, if the detector is only used in between the triangular peaks, the vibrations are expected to be much lower than those estimated.
 | 
			
		||||
@@ -758,8 +759,9 @@ The results of this simulation will be compared to simulations using the NASS in
 | 
			
		||||
An 3D animation of the simulation is shown in Figure [[fig:open_loop_sim]].
 | 
			
		||||
 | 
			
		||||
A zoom in the micro-meter ranger on the sample's location is shown in Figure [[fig:open_loop_sim_zoom]] with two frames:
 | 
			
		||||
- a non-rotating frame corresponding to the wanted position of the sample.
 | 
			
		||||
  Note that this frame is moving with the granite.
 | 
			
		||||
- a non-rotating frame corresponding to the focusing point of the X-ray.
 | 
			
		||||
  It does in that case correspond to the wanted position of the sample.
 | 
			
		||||
  Note that this frame is moving with the granite as the nano-focusing optics are fixed to the granite.
 | 
			
		||||
- a rotating frame that corresponds to the actual pose of the sample
 | 
			
		||||
 | 
			
		||||
The motion of the sample follows the wanted motion but with vibrations in the micro-meter range as was expected.
 | 
			
		||||
@@ -803,17 +805,20 @@ In the next sections, it will allows to optimally design the nano-hexapod, to de
 | 
			
		||||
<<sec:nano_hexapod_design>>
 | 
			
		||||
 | 
			
		||||
** Introduction                                                      :ignore:
 | 
			
		||||
As explain before, the nano-hexapod properties (mass, stiffness, architecture, ...) will influence:
 | 
			
		||||
As explain before, the nano-hexapod properties (mass, stiffness, legs' orientation, ...) will influence:
 | 
			
		||||
- the effect of disturbances $G_d$ (important for the rejection of disturbances)
 | 
			
		||||
- the plant dynamics $G$ (important for the control robustness properties)
 | 
			
		||||
 | 
			
		||||
Thus, we here wish to find the optimal nano-hexapod properties such that:
 | 
			
		||||
- the effect of disturbances is minimized (Section [[sec:optimal_stiff_dist]])
 | 
			
		||||
- the plant uncertainty due to a change of payload mass and experimental conditions is minimized (Section [[sec:optimal_stiff_plant]])
 | 
			
		||||
- the plant has nice dynamical properties for control (Section [[sec:nano_hexapod_architecture]])
 | 
			
		||||
 | 
			
		||||
The study presented here only consider changes in the nano-hexapod *stiffness* for two reasons:
 | 
			
		||||
- the nano-hexapod mass cannot be change too much, and will anyway be negligible compare to the metrology reflector and the payload masses
 | 
			
		||||
- 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
 | 
			
		||||
In this study, the effect of the nano-hexapod's mass characteristics is not taken into account because:
 | 
			
		||||
1. it cannot be changed a lot
 | 
			
		||||
2. it is quite negligible compare the to metrology reflector and the payload's masses that is fixed to nano-hexapod's top platform
 | 
			
		||||
 | 
			
		||||
Also, the effect of the nano-hexapod's damping properties will be studied when applying active damping techniques.
 | 
			
		||||
 | 
			
		||||
** Optimal Stiffness to reduce the effect of disturbances
 | 
			
		||||
<<sec:optimal_stiff_dist>>
 | 
			
		||||
@@ -1043,6 +1048,127 @@ This show how the dynamics evolves with the stiffness and how different effects
 | 
			
		||||
  In such case, the main limitation will be heavy samples with small stiffnesses.
 | 
			
		||||
#+end_important
 | 
			
		||||
 | 
			
		||||
** Nano-Hexapod Architecture
 | 
			
		||||
<<sec:nano_hexapod_architecture>>
 | 
			
		||||
 | 
			
		||||
*** Introduction                                                    :ignore:
 | 
			
		||||
 | 
			
		||||
*** Kinematic Analysis - Jacobian Matrix
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
The kinematic analysis of a parallel manipulator is well described in cite:taghirad13_paral:
 | 
			
		||||
#+begin_quote
 | 
			
		||||
Kinematic analysis refers to the study of the geometry of motion of a robot, without considering the forces an torques that cause the motion.
 | 
			
		||||
In this analysis, the relation between the geometrical parameters of the manipulator with the final motion of the moving platform is derived and analyzed.
 | 
			
		||||
#+end_quote
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
From cite:taghirad13_paral:
 | 
			
		||||
#+begin_quote
 | 
			
		||||
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*.
 | 
			
		||||
#+end_quote
 | 
			
		||||
 | 
			
		||||
The Jacobian matrix $\bm{\mathcal{J}}$ can be computed form the orientation of the legs and the position of the flexible joints.
 | 
			
		||||
 | 
			
		||||
If we note:
 | 
			
		||||
- $\delta\bm{\mathcal{L}} = [ \delta l_1, \delta l_2, \delta l_3, \delta l_4, \delta l_5, \delta l_6 ]^T$: the vector of small legs' displacements
 | 
			
		||||
- $\delta \bm{\mathcal{X}} = [\delta x, \delta y, \delta z, \delta \theta_x, \delta \theta_y, \delta \theta_z ]^T$: the vector of small mobile platform displacements
 | 
			
		||||
 | 
			
		||||
The Jacobian matrix links the two vectors:
 | 
			
		||||
\begin{align*}
 | 
			
		||||
  \delta\bm{\mathcal{L}} &= \bm{J} \delta\bm{\mathcal{X}} \\
 | 
			
		||||
  \delta\bm{\mathcal{X}} &= \bm{J}^{-1} \delta\bm{\mathcal{L}}
 | 
			
		||||
\end{align*}
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
If we note:
 | 
			
		||||
- $\bm{\tau} = [\tau_1, \tau_2, \cdots, \tau_6]^T$: vector of actuator forces applied in each strut
 | 
			
		||||
- $\bm{\mathcal{F}} = [\bm{f}, \bm{n}]^T$: external force/torque action on the mobile platform
 | 
			
		||||
 | 
			
		||||
\begin{equation*}
 | 
			
		||||
  \bm{\mathcal{F}} = \bm{J}^T \bm{\tau}
 | 
			
		||||
\end{equation*}
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
\begin{equation*}
 | 
			
		||||
  \bm{\mathcal{F}} = \bm{K} \delta \bm{\mathcal{X}}
 | 
			
		||||
\end{equation*}
 | 
			
		||||
 | 
			
		||||
\begin{equation*}
 | 
			
		||||
  \bm{K} = \bm{J}^T \mathcal{K} \bm{J}
 | 
			
		||||
\end{equation*}
 | 
			
		||||
\begin{equation*}
 | 
			
		||||
  \bm{C} = \bm{K}^{-1} = (\bm{J}^T \mathcal{K} \bm{J})^{-1}
 | 
			
		||||
\end{equation*}
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
Kinematic Study https://tdehaeze.github.io/stewart-simscape/kinematic-study.html
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
Mobility can be estimated from the architecture of the Stewart platform and the leg's stroke.
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
Stiffness properties is estimated from the architecture and leg's stiffness
 | 
			
		||||
 | 
			
		||||
*** Kinematic Analysis - Mobility
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
#+name: fig:mobility_translations_null_rotation
 | 
			
		||||
#+caption: Figure caption
 | 
			
		||||
[[file:figs/mobility_translations_null_rotation.png]]
 | 
			
		||||
 | 
			
		||||
*** Kinematic Study
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
*** Flexible Joints
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
Active Damping Study https://tdehaeze.github.io/stewart-simscape/control-active-damping.html
 | 
			
		||||
Flexible Joint stiffness => not problematic for the chosen active damping technique
 | 
			
		||||
 | 
			
		||||
#+name: tab:yang19_stiffness_flexible_joints
 | 
			
		||||
#+caption: Stiffness of flexible joints
 | 
			
		||||
| $k_{\theta u},\ k_{\psi u}$ | $72 Nm/rad$ |
 | 
			
		||||
| $k_{\theta s}$              | $51 Nm/rad$ |
 | 
			
		||||
| $k_{\psi s}$                | $62 Nm/rad$ |
 | 
			
		||||
| $k_{\gamma s}$              | $64 Nm/rad$ |
 | 
			
		||||
 | 
			
		||||
#+name: fig:preumont07_flexible_joints
 | 
			
		||||
#+caption: Figure caption cite:preumont07_six_axis_singl_stage_activ
 | 
			
		||||
[[file:figs/preumont07_flexible_joints.png]]
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
#+name: fig:yang19_flexible_joints
 | 
			
		||||
#+caption: Figure caption
 | 
			
		||||
[[file:figs/yang19_flexible_joints.png]]
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
*** Cubic Architecture
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
Study of cubic architecture https://tdehaeze.github.io/stewart-simscape/cubic-configuration.html
 | 
			
		||||
Has some advantages such as uniform stiffness and uniform mobility.
 | 
			
		||||
It can have very nice properties in specific conditions that will not be the case for this application.
 | 
			
		||||
The cubic configuration also puts much restriction on the position and orientation of each leg.
 | 
			
		||||
This configuration is such not recommended.
 | 
			
		||||
 | 
			
		||||
#+name: fig:3d-cubic-stewart-aligned
 | 
			
		||||
#+caption: Figure caption
 | 
			
		||||
[[file:figs/3d-cubic-stewart-aligned.png]]
 | 
			
		||||
 | 
			
		||||
** Conclusion
 | 
			
		||||
#+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.
 | 
			
		||||
@@ -1102,19 +1228,39 @@ The HAC-LAC architecture thus consisted of two cascade controllers:
 | 
			
		||||
** Active Damping and Sensors to be included in the nano-hexapod
 | 
			
		||||
<<sec:lac_control>>
 | 
			
		||||
 | 
			
		||||
Active Damping can help:
 | 
			
		||||
- by reducing the effect of disturbances close to the resonance of the system
 | 
			
		||||
- by making the plant dynamics simpler to control for the High Authority Controller
 | 
			
		||||
 | 
			
		||||
 
 | 
			
		||||
*** Introduction                                                    :ignore:
 | 
			
		||||
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.
 | 
			
		||||
 | 
			
		||||
Because of the rotation of the hexapod,
 | 
			
		||||
 | 
			
		||||
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:
 | 
			
		||||
- the use of force sensors is to be avoided as it could introduce instability in the system due to the nano-hexapod's rotation
 | 
			
		||||
- 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).
 | 
			
		||||
  It would also be difficult to apply in a robust way due to the non-collocation with the actuators
 | 
			
		||||
- 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
 | 
			
		||||
 | 
			
		||||
*** Effect of the Spindle's Rotation
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
#+name: fig:dvf_root_locus_ws
 | 
			
		||||
#+caption: Figure caption
 | 
			
		||||
[[file:figs/dvf_root_locus_ws.png]]
 | 
			
		||||
 | 
			
		||||
#+name: fig:iff_root_locus_ws
 | 
			
		||||
#+caption: Figure caption
 | 
			
		||||
[[file:figs/iff_root_locus_ws.png]]
 | 
			
		||||
 | 
			
		||||
*** Relative Direct Velocity Feedback Architecture
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
Active Damping can help:
 | 
			
		||||
- by reducing the effect of disturbances close to the resonance of the system
 | 
			
		||||
- by making the plant dynamics simpler to control for the High Authority Controller
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
*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]]).
 | 
			
		||||
 | 
			
		||||
@@ -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.
 | 
			
		||||
This may not be the optimal choice as will be further explained.
 | 
			
		||||
 | 
			
		||||
*** 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]].
 | 
			
		||||
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
 | 
			
		||||
[[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]].
 | 
			
		||||
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]]
 | 
			
		||||
 | 
			
		||||
** Simulation of More Complex Experiments
 | 
			
		||||
*** Introduction                                                    :ignore:
 | 
			
		||||
 | 
			
		||||
*** Micro-Hexapod offset
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
#+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]]
 | 
			
		||||
 | 
			
		||||
*** Simultaneous Translation Scans
 | 
			
		||||
:PROPERTIES:
 | 
			
		||||
:UNNUMBERED: t
 | 
			
		||||
:END:
 | 
			
		||||
 | 
			
		||||
#+name: fig:ty_scans
 | 
			
		||||
#+caption: Figure caption
 | 
			
		||||
#+caption: Top View of a tomography experiment combined with translation scans
 | 
			
		||||
[[file:figs/ty_scans.gif]]
 | 
			
		||||
 | 
			
		||||
** Conclusion
 | 
			
		||||
@@ -1281,6 +1446,8 @@ A more complete study of the control of the NASS is performed [[https://tdehaeze
 | 
			
		||||
* General Conclusion and Further notes
 | 
			
		||||
<<sec:conclusion_and_further_notes>>
 | 
			
		||||
 | 
			
		||||
** Nano-Hexapod Specifications
 | 
			
		||||
 | 
			
		||||
** General Conclusion
 | 
			
		||||
 | 
			
		||||
 | 
			
		||||
@@ -1291,8 +1458,10 @@ This should not be significant.
 | 
			
		||||
 | 
			
		||||
** Further Work
 | 
			
		||||
 | 
			
		||||
** Cable Forces
 | 
			
		||||
 | 
			
		||||
** Using soft mounts for the
 | 
			
		||||
 | 
			
		||||
** Using soft mounts for the Granite
 | 
			
		||||
<<sec:soft_granite>>
 | 
			
		||||
 | 
			
		||||
#+name: fig:opt_stiff_soft_granite_Dw
 | 
			
		||||
 
 | 
			
		||||
							
								
								
									
										37
									
								
								ref.bib
									
									
									
									
									
								
							
							
						
						@@ -3,7 +3,6 @@
 | 
			
		||||
  title = {The Design of High Performance Mechatronics - 2nd Revised Edition},
 | 
			
		||||
  year = {2014},
 | 
			
		||||
  publisher = {Ios Press},
 | 
			
		||||
  tags = {favorite},
 | 
			
		||||
}
 | 
			
		||||
 | 
			
		||||
@article{oomen18_advan_motion_contr_precis_mechat,
 | 
			
		||||
@@ -16,7 +15,6 @@
 | 
			
		||||
  year = {2018},
 | 
			
		||||
  doi = {10.1541/ieejjia.7.127},
 | 
			
		||||
  url = {https://doi.org/10.1541/ieejjia.7.127},
 | 
			
		||||
  tags = {favorite},
 | 
			
		||||
}
 | 
			
		||||
 | 
			
		||||
@book{preumont18_vibrat_contr_activ_struc_fourt_edition,
 | 
			
		||||
@@ -28,5 +26,40 @@
 | 
			
		||||
  doi = {10.1007/978-3-319-72296-2},
 | 
			
		||||
  pages = {nil},
 | 
			
		||||
  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},
 | 
			
		||||
}
 | 
			
		||||
 | 
			
		||||
@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},
 | 
			
		||||
}
 | 
			
		||||
 
 | 
			
		||||