diff options
| -rw-r--r-- | paper/rotohsm_paper.pdf | bin | 3564423 -> 3537727 bytes | |||
| -rw-r--r-- | paper/rotohsm_paper.tex | 6 | ||||
| -rw-r--r-- | paper/rotohsm_tech_report.pdf | bin | 112288 -> 112384 bytes |
3 files changed, 3 insertions, 3 deletions
diff --git a/paper/rotohsm_paper.pdf b/paper/rotohsm_paper.pdf Binary files differindex 7ef9489..e9be752 100644 --- a/paper/rotohsm_paper.pdf +++ b/paper/rotohsm_paper.pdf diff --git a/paper/rotohsm_paper.tex b/paper/rotohsm_paper.tex index 6ee3de1..e7650dc 100644 --- a/paper/rotohsm_paper.tex +++ b/paper/rotohsm_paper.tex @@ -690,7 +690,7 @@ fly, without stopping the rotor. \begin{figure} \center - \includegraphics[width=0.7\textwidth]{../../prototype/sensor-analysis/fig-acc-theory-meas-run50.pdf} + \includegraphics[width=0.7\textwidth]{../prototype/sensor-analysis/fig-acc-theory-meas-run50.pdf} \caption{Centrifugal acceleration versus angular frequency in theory and in our experiments. Experimental measurements are shown after correction for device-specific offset and scale error. Our measurements showed good agreement with our theoretical results. Above \SI{300}{rpm}, the relative acceleration error was consistently @@ -702,7 +702,7 @@ fly, without stopping the rotor. \begin{figure} \begin{subfigure}{0.5\textwidth} \center - \includegraphics[width=1.1\textwidth]{../../prototype/sensor-analysis/fig-acc-trace-steps-run50.pdf} + \includegraphics[width=1.1\textwidth]{../prototype/sensor-analysis/fig-acc-trace-steps-run50.pdf} \caption{Raw recording of accelerometer measurements during one experiment run. Shaded areas indicate time intervals when we manually adjusted speed.} \label{fig-acc-steps} @@ -710,7 +710,7 @@ fly, without stopping the rotor. \hfill \begin{subfigure}{0.45\textwidth} \center - \includegraphics[width=1.1\textwidth]{../../prototype/sensor-analysis/fig-acc-trace-stacked-run50.pdf} + \includegraphics[width=1.1\textwidth]{../prototype/sensor-analysis/fig-acc-trace-stacked-run50.pdf} \caption{Valid measurements cropped out from \ref{fig-acc-steps} for various frequencies. Intermodulation artifacts from the accelerometer's $\SI{10}{\hertz}$ sampling frequency and the $\SI{3}{\hertz}$ to $\SI{18}{\hertz}$ rotation frequency due to gravity and device vibration are clearly visible.} diff --git a/paper/rotohsm_tech_report.pdf b/paper/rotohsm_tech_report.pdf Binary files differindex b5cbade..93dac75 100644 --- a/paper/rotohsm_tech_report.pdf +++ b/paper/rotohsm_tech_report.pdf |