Add notes on actuator stroke and force
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@ -2042,7 +2042,9 @@ In this section are gathered all the specifications related to the nano-hexapod.
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The wanted dimension of the nano-hexapod are shown in Figure [[fig:nano_hexapod_size]]:
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The wanted dimension of the nano-hexapod are shown in Figure [[fig:nano_hexapod_size]]:
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- Diameter of the bottom platform: 300mm
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- Diameter of the bottom platform: 300mm
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- Diameter of the top platform: 200mm
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- Diameter of the top platform: 200mm
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- Maximum Height: 90mm
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- *Maximum Height: 90mm*
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The limiting height might be quite problematic for the integration of the flexible joints, the actuators and sensors.
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#+name: fig:nano_hexapod_size
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#+name: fig:nano_hexapod_size
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#+caption: First implementation of the nano-hexapod / metrology reflector and sample interface
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#+caption: First implementation of the nano-hexapod / metrology reflector and sample interface
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@ -2063,27 +2065,49 @@ The required angular stroke has not been estimated in this study.
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It is however simple to do so as the angular motion of each joint can easily be measured in the multi-body model used to perform the simulations.
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It is however simple to do so as the angular motion of each joint can easily be measured in the multi-body model used to perform the simulations.
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Typical angular stroke for such flexible joints is expected.
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Typical angular stroke for such flexible joints is expected.
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*** Actuators
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*** Strut Stiffness
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:PROPERTIES:
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:PROPERTIES:
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:UNNUMBERED: t
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:UNNUMBERED: t
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:END:
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:END:
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The actuation part is probably the most important part of the Stewart platform.
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- Stiffness:
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- Resonances should stay between 5Hz and 50Hz for payload masses up to 50kg
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- Resonances should stay between 5Hz and 50Hz for payload masses up to 50kg
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- This corresponds to strut stiffnesses of $k \approx 10^5 - 10^6\,[N/m]$
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- This corresponds to strut stiffnesses of $k \approx 10^5 - 10^6\,[N/m]$
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- Force:
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- Weight: $60\,kg \rightarrow 600\,N \rightarrow 60\,N$ on each actuator
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*** Actuator Force
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- Dynamic: few Newtons
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:PROPERTIES:
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- Estimation of the required stroke:
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:UNNUMBERED: t
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- From simulation (i.e. for disturbance rejection alone), $\pm 5 \mu m$
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:END:
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- However, the required stroke probably depends on two other factors:
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- Static positioning errors of the stages
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Based on simulations:
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- Maximum tracking errors of the stages (mainly translation stage and tilt stage).
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- Continuous Force: $\pm 5\,[N]$ (due to centrifugal forces)
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This is probably more difficult to obtain.
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- "Variable" Force: $\pm 1\,[N]$
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If static deflection is to be compensated by the actuator, $\approx 100\,[N]$ of continuous force is required for each actuator.
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*** Actuator Stroke
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:PROPERTIES:
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:UNNUMBERED: t
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:END:
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Based on simulations, the required actuator stroke seems to be $\pm 5\,[\mu m]$.
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This however does not take into account two error types that will have to be compensated by the nano-hexapod:
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- the static positioning errors of all the micro-station's stages.
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These errors have been measured by Hans-Peter, and are in the order of tens of $\mu m$ and tens of $\mu rad$.
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- the tracking errors of the translation stage and tilt stage.
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This is probably more difficult to estimate.
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However, by limiting the acceleration of these stages, we may limit the dynamic tracking errors to acceptable levels
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However, by limiting the acceleration of these stages, we may limit the dynamic tracking errors to acceptable levels
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- If the chosen technology allows $\pm 50 \mu m$ that would be safer
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Some security margin should be taken as if the nano-hexapod has not enough stroke to compensated the above errors, the system will not be able to compensate all the vibrations.
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Thus, an actuator stroke of $\pm 50 \mu m$ would be quite safe.
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Note that a piezoelectric stack have a maximum strain of $0.1\%$.
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A piezo stack with a stroke of $\pm 50\,[\mu m]$ will have a length size of $\approx 100\,[mm]$ making it difficult to integrate in the nano-hexapod.
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*** Sensors
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*** Sensors
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:PROPERTIES:
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:PROPERTIES:
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