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It is important to resolve the coupled dynamics, in order to avoid large oscillations and instabilities.
In general, the AD state cannot persist when wave condition changes, usually leaping to large oscillations.
Flutter instability and large oscillations occur under the aerodynamic moment, which provides "negative damping".
These results are used to suggest simple means of controlling or minimizing the large oscillations.
In particular, the potential isodynamical to sufficiently large oscillations on a double valley shaped track has a triple well form.
In many simulations these effects cause large oscillations of the velocity close to the interface, so-called spurious velocities.
PI controllers would need to operate under very high gain settings to achieve an equally fast rise, however, this would inevitably result in large oscillations around the target levels (Supplementary Note 4). Figure 2: Tracking of reference sfGFP expression trajectories.
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The present results are valid for small as well as large oscillation amplitudes.
This method is valid for both small and large parameters and large oscillation amplitude.
The statistical results show a large oscillation under transverse wind velocities.
The results are valid for small as well as large oscillation amplitudes.
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