Rename footnotes
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@ -265,8 +265,8 @@ To do so, a precisely machined mounting tool (Figure ref:fig:test_nhexa_center_p
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#+end_subfigure
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#+end_figure
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The mechanical tolerances of the received plates were checked using a FARO arm[fn:1] (Figure ref:fig:test_nhexa_plates_tolerances) and were found to comply with the requirements[fn:2].
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The same was done for the mounting tool[fn:3].
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The mechanical tolerances of the received plates were checked using a FARO arm[fn:test_nhexa_1] (Figure ref:fig:test_nhexa_plates_tolerances) and were found to comply with the requirements[fn:test_nhexa_2].
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The same was done for the mounting tool[fn:test_nhexa_3].
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The two plates were then fixed to the mounting tool, as shown in Figure ref:fig:test_nhexa_mounting_tool_hexapod_top_view.
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The main goal of this "mounting tool" is to position the flexible joint interfaces (the "V" shapes) of both plates so that a cylinder can rest on the 4 flat interfaces at the same time.
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@ -293,7 +293,7 @@ The main goal of this "mounting tool" is to position the flexible joint interfac
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The quality of the positioning can be estimated by measuring the "straightness" of the top and bottom "V" interfaces.
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This corresponds to the diameter of the smallest cylinder which contains all points along the measured axis.
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This was again done using the FARO arm, and the results for all six struts are summarized in Table ref:tab:measured_straightness.
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The straightness was found to be better than $15\,\mu m$ for all struts[fn:4], which is sufficiently good to not induce significant stress of the flexible joint during assembly.
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The straightness was found to be better than $15\,\mu m$ for all struts[fn:test_nhexa_4], which is sufficiently good to not induce significant stress of the flexible joint during assembly.
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#+name: tab:measured_straightness
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#+caption: Measured straightness between the two "V" shapes for the six struts. These measurements were performed twice for each strut.
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@ -395,8 +395,8 @@ Finally, the multi-body model representing the suspended table was tuned to matc
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<<ssec:test_nhexa_table_setup>>
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The design of the suspended table is quite straightforward.
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First, an optical table with high frequency flexible mode was selected[fn:5].
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Then, four springs[fn:6] were selected with low spring rate such that the suspension modes are below 10Hz.
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First, an optical table with high frequency flexible mode was selected[fn:test_nhexa_5].
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Then, four springs[fn:test_nhexa_6] were selected with low spring rate such that the suspension modes are below 10Hz.
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Finally, some interface elements were designed, and mechanical lateral mechanical stops were added (Figure ref:fig:test_nhexa_suspended_table_cad).
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#+name: fig:test_nhexa_suspended_table_cad
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@ -407,7 +407,7 @@ Finally, some interface elements were designed, and mechanical lateral mechanica
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** Modal analysis of the suspended table
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<<ssec:test_nhexa_table_identification>>
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In order to perform a modal analysis of the suspended table, a total of 15 3-axis accelerometers[fn:7] were fixed to the breadboard.
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In order to perform a modal analysis of the suspended table, a total of 15 3-axis accelerometers[fn:test_nhexa_7] were fixed to the breadboard.
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Using an instrumented hammer, the first 9 modes could be identified and are summarized in Table ref:tab:test_nhexa_suspended_table_modes.
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The first 6 modes are suspension modes (i.e. rigid body mode of the breadboard) and are located below 10Hz.
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The next modes are the flexible modes of the breadboard as shown in Figure ref:fig:test_nhexa_table_flexible_modes, and are located above 700Hz.
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@ -2159,10 +2159,10 @@ end
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* Footnotes
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[fn:7]PCB 356B18. Sensitivity is $1\,V/g$, measurement range is $\pm 5\,g$ and bandwidth is $0.5$ to $5\,\text{kHz}$.
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[fn:6]"SZ8005 20 x 044" from Steinel. The spring rate is specified at $17.8\,N/mm$
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[fn:5]The 450 mm x 450 mm x 60 mm Nexus B4545A from Thorlabs.
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[fn:4]As the accuracy of the FARO arm is $\pm 13\,\mu m$, the true straightness is probably better than the values indicated. The limitation of the instrument is here reached.
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[fn:3]The height dimension is better than $40\,\mu m$. The diameter fitting of 182g6 and 24g6 with the two plates is verified.
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[fn:2]Location of all the interface surfaces with the flexible joints were checked. The fittings (182H7 and 24H8) with the interface element were also checked.
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[fn:1]FARO Arm Platinum 4ft, specified accuracy of $\pm 13\mu m$
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[fn:test_nhexa_7]PCB 356B18. Sensitivity is $1\,V/g$, measurement range is $\pm 5\,g$ and bandwidth is $0.5$ to $5\,\text{kHz}$.
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[fn:test_nhexa_6]"SZ8005 20 x 044" from Steinel. The spring rate is specified at $17.8\,N/mm$
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[fn:test_nhexa_5]The 450 mm x 450 mm x 60 mm Nexus B4545A from Thorlabs.
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[fn:test_nhexa_4]As the accuracy of the FARO arm is $\pm 13\,\mu m$, the true straightness is probably better than the values indicated. The limitation of the instrument is here reached.
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[fn:test_nhexa_3]The height dimension is better than $40\,\mu m$. The diameter fitting of 182g6 and 24g6 with the two plates is verified.
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[fn:test_nhexa_2]Location of all the interface surfaces with the flexible joints were checked. The fittings (182H7 and 24H8) with the interface element were also checked.
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[fn:test_nhexa_1]FARO Arm Platinum 4ft, specified accuracy of $\pm 13\mu m$
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