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@@ -39,14 +39,14 @@ In the frequency range that is relevant for control, the dynamical behavior is m
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In particular, the mechanics can typically be described as:
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\begin{equation}
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G\_m = \sum\_{i=1}^{n\_{RB}} \frac{c\_i b\_i^T}{s^2} + \sum\_{n\_{RB} + 1}^{n\_s} \frac{c\_i b\_i^T}{s^2 + 2\xi \omega\_i s + \omega\_i^2}
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G\_m = \sum\_{i=1}^{n\_{RB}} \frac{c\_i b\_i^T}{s^2} + \sum\_{n\_{RB} + 1}^{n\_s} \frac{c\_i b\_i^T}{s^2 + 2\zeta \omega\_i s + \omega\_i^2}
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\end{equation}
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where the first term refers to rigid body modes and the second term to flexible modes.
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- \\(n\_{RB}\\) is the number of rigid body modes
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- \\(c\_i \in \mathbb{R}^{n\_y}\\) and \\(b\_i \in \mathbb{R}^{n\_u}\\) are associated with the mode shapes
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- \\(\xi\_i, \omega\_i \in \mathbb{R}\_+\\)
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- \\(\zeta\_i, \omega\_i \in \mathbb{R}\_+\\)
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In traditional positioning systems, the number of actuators \\(n\_u\\) and sensors \\(n\_y\\) equals the number of rigid body modes \\(n\_{RB}\\) and are positioned such that the matrix \\(\sum\_{i=1}^{n\_{RB}} c\_i b\_i^T\\) is invertible.
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In this case, matrices \\(T\_u\\) and \\(T\_y\\) can be selected such that:
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