## 3 Results
### Pelvis Motion  
During both the loading and landing phases, pelvis motion was not significantly different between dominant and non-dominant legs (Table 3). In preparation for taking-off, the pelvis was found to extend (sagittal plane), adduct (frontal plane), and externally rotate (transverse plane). On landing, the pelvis was found to extend, abduct, and internally rotate.  
\begin{table}
\begin{tabular}{l l c c c c} \hline \hline  & & \multicolumn{2}{c}{**Non-Dominant Limb**} & \multicolumn{2}{c}{**Dominant Limb**} \\ \cline{3-6}
**Phase** & **Variable** & & & **ICC [95\% CI]** & **SEM** & **ICC [95\% CI]** & **SEM** \\  & & **ICC [95\% CI]** & & **(Dominant)** & **SEM** \\ \hline Loading & Peak Flexion (degs) & 0.83 [0.68–0.93] & 1.56 & 0.83 [0.68–0.94] & 1.55 \\  & Peak Adduction (degs) & 0.89 [0.77–0.96] & 0.63 & 0.83 [0.67–0.93] & 1.28 \\  & Peak Abduction (degs) & 0.87 [0.74–0.95] & 0.92 & 0.90 [0.80–0.96] & 0.58 \\  & Time Peak Add (\%SC) & - & - & - & - \\  & Time Peak Abd (\%SC) & - & - & - & - \\ \hline Landing & Peak Extension (degs) & 0.70 [0.47–0.87] & 1.44 & 0.78 [0.59–0.91] & 1.03 \\  & Peak Flexion (degs) & 0.73 [0.52–0.89] & 2.35 & 0.77 [0.58–0.91] & 1.96 \\  & Peak Adduction (degs) & 0.86 [0.73–0.95] & 0.66 & 0.79 [0.61–0.92] & 1.26 \\  & Peak Abduction (degs) & 0.87 [0.75–0.95] & 0.81 & 0.92 [0.83–0.97] & 0.44 \\  & Time Peak Add (\%SC) & - & - & - & - \\  & Time Peak Abd (\%SC) & - & - & - & - \\ \hline ICC 0.5–0.75 = moderate reliability, ICC 0.75–0.90 = good reliability, \& ICC \(>0.90\) = excellent reliability. Larger SEM indicates less reliability. & & & \\ \hline \end{tabular}
\end{table}
Table 1: Reliability measures.  
\begin{table}
\begin{tabular}{l l c c c c c} \hline \hline
**Phase** & **Variable** & **Non-Dominant** & **Dominant** & **\(p\)-Value** & **Mean Diff [95\% CI]** & **Effect Size (d)** \\ \hline Loading & Peak Flexion (degs) & \(-58.2\pm 9.2\) & \(-59.7\pm 9.1\) & 0.67 & 1.5 [15.2, –12.2] & 0.16 \\  & Peak Adduction (degs) & \(-0.3\pm 5.7\) & \(4.6\pm 7.5\) & 0.06 & 5.0 [14.2, –4.3] & 0.75 \\  & Peak Abduction (degs) & \(-8.2\pm 7.1\) & \(-0.8\pm 5.8\) & 0.01 * & 7.3 [17.0, –2.3] & 1.13 \\  & Time Peak Add (\%SC) & \(22\pm 25\) & \(30\pm 24\) & 0.39 & 7.9 [42.3, –26.4] & 0.32 \\  & Time Peak Abd (\%SC) & \(77\pm 23\) & \(67\pm 29\) & 0.33 & 9.9 [47.9, –27.9] & 0.38 \\ \hline Landing & Peak Extension (degs) & \(-13.8\pm 4.7\) & \(-11.3\pm 4.7\) & 0.16 & 2.5 [9.2, –4.1] & 0.53 \\  & Peak Flexion (degs) & \(-47.8\pm 8.7\) & \(-46.1\pm 8.5\) & 0.61 & 1.7 [14.2, –10.9] & 0.20 \\  & Peak Adduction (degs) & \(2.8\pm 4.7\) & \(7.0\pm 6.0\) & 0.05 * & 4.2 [11.7, –3.3] & 0.79 \\  & Peak Abduction (degs) & \(-8.7\pm 6.2\) & \(-2.2\pm 5.5\) & 0.01 * & 6.5 [15.0, –2.0] & 1.11 \\  & Time Peak Add (\%SC) & \(16\pm 18\) & \(23\pm 24\) & 0.46 & 6.1 [36.9, –24.8] & 0.29 \\  & Time Peak Abd (\%SC) & \(72\pm 20\) & \(62\pm 31\) & 0.33 & 9.9 [47.3, –27.5] & 0.39 \\ \hline \end{tabular}
\begin{tabular}{l c c c c} \hline \hline \multicolumn{2}{c}{Mean \(\pm\) Standard Deviation. * Significant at \(p\leq 0.05\). [PERSON]’s d calculated for effect size (0.2–0.5 are considered} \\ \multicolumn{2}{c}{small, 0.5–0.8 considered moderate, and \(>\)0.8 considered a large effect).} \\ \end{tabular}
\end{table}
Table 2: Knee motion for both loading and landing phases. Abd—Abduction; Add—Adduction.