Update some typography
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@ -61,7 +61,7 @@ As the translation stage is rotating around the Z axis due to the spindle, the f
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The measurement is either the $x-y$ displacement of the object located on top of the translation stage or the $u-v$ displacement of the sample with respect to a fixed reference frame.
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#+name: fig:rotating_frame_2dof
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#+caption: Schematic of the mecanical system
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#+caption: Schematic of the mechanical system
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[[./figs/rotating_frame_2dof.png]]
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In the following block diagram:
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@ -79,7 +79,7 @@ Indices $u$ and $v$ corresponds to signals in the rotating reference frame ($\ve
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- $\epsilon_u$ and $\epsilon_v$ are position error of the sample along $\vec{i}_u$ and $\vec{i}_v$
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** Equations
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<<sec:equations>>
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<<sec:equations>>
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Based on the figure [[fig:rotating_frame_2dof]], we can write the equations of motion of the system.
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Let's express the kinetic energy $T$ and the potential energy $V$ of the mass $m$:
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@ -111,7 +111,7 @@ F_{\text{ext}, x} &= F_u \cos{\theta} - F_v \sin{\theta}\\
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F_{\text{ext}, y} &= F_u \sin{\theta} + F_v \cos{\theta}
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\end{align*}
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By appling the Lagrangian equations, we obtain:
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By applying the Lagrangian equations, we obtain:
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\begin{align}
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m\ddot{x} + kx = F_u \cos{\theta} - F_v \sin{\theta}\\
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m\ddot{y} + ky = F_u \sin{\theta} + F_v \cos{\theta}
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@ -125,6 +125,11 @@ y & = d_u \sin{\theta} + d_v \cos{\theta}
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We obtain:
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\begin{align*}
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\dot{x} & = \dot{d_u} \cos{\theta} - d_u\dot{\theta}\sin{\theta} - \dot{d_v}\sin{\theta} - d_v\dot{\theta} \cos{\theta} \\
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\dot{y} & = \dot{d_u} \sin{\theta} + d_u\dot{\theta}\cos{\theta} + \dot{d_v}\cos{\theta} - d_v\dot{\theta} \sin{\theta}
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\end{align*}
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and:
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\begin{align*}
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\ddot{x} & = \ddot{d_u} \cos{\theta} - 2\dot{d_u}\dot{\theta}\sin{\theta} - d_u\ddot{\theta}\sin{\theta} - d_u\dot{\theta}^2 \cos{\theta}
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- \ddot{d_v} \sin{\theta} - 2\dot{d_v}\dot{\theta}\cos{\theta} - d_v\ddot{\theta}\cos{\theta} + d_v\dot{\theta}^2 \sin{\theta} \\
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\ddot{y} & = \ddot{d_u} \sin{\theta} + 2\dot{d_u}\dot{\theta}\cos{\theta} + d_u\ddot{\theta}\cos{\theta} - d_u\dot{\theta}^2 \sin{\theta}
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@ -133,21 +138,26 @@ We obtain:
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By injecting the previous result into the Lagrangian equation, we obtain:
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\begin{align*}
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m \ddot{d_u} \cos{\theta} - 2m\dot{d_u}\dot{\theta}\sin{\theta} - m d_u\ddot{\theta}\sin{\theta} - m d_u\dot{\theta}^2 \cos{\theta}
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-m \ddot{d_v} \sin{\theta} - 2m\dot{d_v}\dot{\theta}\cos{\theta} - m d_v\ddot{\theta}\cos{\theta} + m d_v\dot{\theta}^2 \sin{\theta}
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m \ddot{d_u} \cos{\theta} - 2m\dot{d_u}\dot{\theta}\sin{\theta} - m d_u\ddot{\theta}\sin{\theta} - m d_u\dot{\theta}^2 \cos{\theta}
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- m \ddot{d_v} \sin{\theta} - 2m\dot{d_v}\dot{\theta}\cos{\theta} - m d_v\ddot{\theta}\cos{\theta} + m d_v\dot{\theta}^2 \sin{\theta}
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+ c \dot{d_u} \cos{\theta} - c d_u\dot{\theta}\sin{\theta} - c \dot{d_v}\sin{\theta} - c d_v\dot{\theta} \cos{\theta}
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+ k d_u \cos{\theta} - k d_v \sin{\theta} = F_u \cos{\theta} - F_v \sin{\theta} \\
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m \ddot{d_u} \sin{\theta} + 2m\dot{d_u}\dot{\theta}\cos{\theta} + m d_u\ddot{\theta}\cos{\theta} - m d_u\dot{\theta}^2 \sin{\theta}
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+ m \ddot{d_v} \cos{\theta} - 2m\dot{d_v}\dot{\theta}\sin{\theta} - m d_v\ddot{\theta}\sin{\theta} - m d_v\dot{\theta}^2 \cos{\theta}
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+ c \dot{d_u} \sin{\theta} + c d_u\dot{\theta}\cos{\theta} + c \dot{d_v}\cos{\theta} - c d_v\dot{\theta} \sin{\theta}
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+ k d_u \sin{\theta} + k d_v \cos{\theta} = F_u \sin{\theta} + F_v \cos{\theta}
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\end{align*}
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Which is equivalent to:
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\begin{align*}
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m \ddot{d_u} - 2m\dot{d_u}\dot{\theta}\frac{\sin{\theta}}{\cos{\theta}} - m d_u\ddot{\theta}\frac{\sin{\theta}}{\cos{\theta}} - m d_u\dot{\theta}^2
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-m \ddot{d_v} \frac{\sin{\theta}}{\cos{\theta}} - 2m\dot{d_v}\dot{\theta} - m d_v\ddot{\theta} + m d_v\dot{\theta}^2 \frac{\sin{\theta}}{\cos{\theta}}
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m \ddot{d_u} - 2m\dot{d_u}\dot{\theta}\frac{\sin{\theta}}{\cos{\theta}} - m d_u\ddot{\theta}\frac{\sin{\theta}}{\cos{\theta}} - m d_u\dot{\theta}^2
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- m \ddot{d_v} \frac{\sin{\theta}}{\cos{\theta}} - 2m\dot{d_v}\dot{\theta} - m d_v\ddot{\theta} + m d_v\dot{\theta}^2 \frac{\sin{\theta}}{\cos{\theta}}
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+ c \dot{d_u} - c d_u\dot{\theta}\frac{\sin{\theta}}{\cos{\theta}} - c \dot{d_v}\frac{\sin{\theta}}{\cos{\theta}} - c d_v\dot{\theta}
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+ k d_u - k d_v \frac{\sin{\theta}}{\cos{\theta}} = F_u - F_v \frac{\sin{\theta}}{\cos{\theta}} \\
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m \ddot{d_u} + 2m\dot{d_u}\dot{\theta}\frac{\cos{\theta}}{\sin{\theta}} + m d_u\ddot{\theta}\frac{\cos{\theta}}{\sin{\theta}} - m d_u\dot{\theta}^2
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+ m \ddot{d_v} \frac{\cos{\theta}}{\sin{\theta}} - 2m\dot{d_v}\dot{\theta} - m d_v\ddot{\theta} - m d_v\dot{\theta}^2 \frac{\cos{\theta}}{\sin{\theta}}
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+ c \dot{d_u} + c d_u\dot{\theta}\frac{\cos{\theta}}{\sin{\theta}} + c \dot{d_v}\frac{\cos{\theta}}{\sin{\theta}} - c d_v\dot{\theta}
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+ k d_u + k d_v \frac{\cos{\theta}}{\sin{\theta}} = F_u + F_v \frac{\cos{\theta}}{\sin{\theta}}
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\end{align*}
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@ -155,11 +165,11 @@ We can then subtract and add the previous equations to obtain the following equa
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#+begin_important
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#+NAME: eq:du_coupled
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\begin{equation}
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m \ddot{d_u} + (k - m\dot{\theta}^2) d_u = F_u + 2 m\dot{d_v}\dot{\theta} + m d_v\ddot{\theta}
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m \ddot{d}_{u} + c \dot{d}_{u} + (k - m\dot{\theta}^2) d_u = F_u + 2 m\dot{d}_v\dot{\theta} + m d_v\ddot{\theta} + c d_{v} \dot{\theta}
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\end{equation}
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#+NAME: eq:dv_coupled
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\begin{equation}
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m \ddot{d_v} + (k - m\dot{\theta}^2) d_v = F_v - 2 m\dot{d_u}\dot{\theta} - m d_u\ddot{\theta}
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m \ddot{d}_{v} + c \dot{d}_{v} + (k - m\dot{\theta}^2) d_v = F_v - 2 m\dot{d}_u\dot{\theta} - m d_u\ddot{\theta} - c d_{u} \dot{\theta}
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\end{equation}
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#+end_important
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@ -272,12 +282,13 @@ This is definitely negligible when using piezoelectric actuators. It may not be
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| Neg. Spring | 1381.7[N/m] | 0.9[N/m] |
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** Limitations due to coupling
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*** Equations
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To simplify, we consider a constant rotating speed $\dot{\theta} = \omega_0$ and thus $\ddot{\theta} = 0$.
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From equations [[eq:du_coupled]] and [[eq:dv_coupled]], we obtain:
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\begin{align*}
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(m s^2 + (k - m{\omega_0}^2)) d_u &= F_u + 2 m {\omega_0} s d_v \\
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(m s^2 + (k - m{\omega_0}^2)) d_v &= F_v - 2 m {\omega_0} s d_u \\
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(m s^2 + c s + (k - m{\omega_0}^2)) d_u &= F_u + 2 m \omega_0 s d_v + c \omega_0 d_v \\
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(m s^2 + c s + (k - m{\omega_0}^2)) d_v &= F_v - 2 m \omega_0 s d_u - c \omega_0 d_v
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\end{align*}
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From second equation:
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@ -303,10 +314,10 @@ The two previous equations can be written in a matrix form:
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#+NAME: eq:coupledplant
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\begin{equation}
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\begin{bmatrix} d_u \\ d_v \end{bmatrix} =
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\frac{1}{(m s^2 + (k - m{\omega_0}^2))^2 + (2 m {\omega_0} s)^2}
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\frac{1}{(m s^2 + cs + (k - m{\omega_r}^2))^2 + (2 m {\omega_r} s + c \omega_r)^2}
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\begin{bmatrix}
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ms^2 + (k-m{\omega_0}^2) & 2 m \omega_0 s \\
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-2 m \omega_0 s & ms^2 + (k-m{\omega_0}^2) \\
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ms^2 + cs + (k-m{\omega_r}^2) & 2 m \omega_r s + c \omega_r \\
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-2 m \omega_r s + c \omega_r & ms^2 + cs + (k-m{\omega_r}^2)
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\end{bmatrix}
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\begin{bmatrix} F_u \\ F_v \end{bmatrix}
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\end{equation}
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@ -411,6 +422,7 @@ From this analysis, we can determine the lowest practical stiffness that is poss
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| k min [N/m] | 2199 | 89 |
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** Effect of rotation speed on the plant
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*** Introduction :ignore:
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As shown in equation [[eq:coupledplant]], the plant changes with the rotation speed $\omega_0$.
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Then, we compute the bode plot of the direct term and coupling term for multiple rotating speed.
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