| Literature DB >> 35891095 |
Jungyeon Choi1, Brian A Knarr2, Yeongjin Gwon3, Jong-Hoon Youn1.
Abstract
Due to a ship's extreme motion, there is a risk of injuries and accidents as people may become unbalanced and be injured or fall from the ship. Thus, individuals must adjust their movements when walking in an unstable environment to avoid falling or losing balance. A person's ability to control their center of mass (COM) during lateral motion is critical to maintaining balance when walking. Dynamic balancing is also crucial to maintain stability while walking. The margin of stability (MOS) is used to define this dynamic balancing. This study aimed to develop a model for predicting balance control and stability in walking on ships by estimating the peak COM excursion and MOS variability using accelerometers. We recruited 30 healthy individuals for this study. During the experiment, participants walked for two minutes at self-selected speeds, and we used a computer-assisted rehabilitation environment (CAREN) system to simulate the roll motion. The proposed prediction models in this study successfully predicted the peak COM excursion and MOS variability. This study may be used to protect and save seafarers or passengers by assessing the risk of balance loss.Entities:
Keywords: CAREN; accelerometer; center of mass; gait stability; margin of stability; ship rolling
Mesh:
Year: 2022 PMID: 35891095 PMCID: PMC9320816 DOI: 10.3390/s22145416
Source DB: PubMed Journal: Sensors (Basel) ISSN: 1424-8220 Impact factor: 3.847
Participants’ demographics.
| Characteristics | Mean ± Standard Deviation |
|---|---|
| Gender (male/female) | 20/10 |
| Age (years) | 30.3 ± 6.1 |
| Height (cm) | 173.0 ± 9.4 |
| Weight (kg) | 71.9 ± 14.5 |
| Body Mass Index (BMI) (kg/m2) | 23.8 ± 3.4 |
Figure 1Experimental settings: (a) placement of reflective markers and IMU sensors; (b) example of simulated roll.
Description of extracted features.
| Feature | Description |
|---|---|
| M | Whole step vector magnitude |
| M10 | Initial 10% step vector magnitude |
| LM | Lateral vector magnitude during a whole step |
| VM | Vertical vector magnitude during a whole step |
| AM | Anterior–posterior vector magnitude during a whole step |
| MD | Vector magnitude during double stance |
| LMD | Lateral vector magnitude during double stance |
| VMD | Vertical vector magnitude during double stance |
| AMD | Anterior-posterior vector magnitude during double stance |
| M30 | Vector magnitude during mid-stance |
| LM30 | Lateral vector magnitude during mid-stance |
| VM30 | Vertical vector magnitude during mid-stance |
| AM30 | Anterior–posterior vector magnitude during mid-stance |
| LHM | Lateral heel-strike magnitude |
| LHS | Standard deviation of lateral acceleration during initial 10% step |
| VHM | Vertical heel-strike magnitude |
| VHS | Standard deviation of vertical acceleration during initial 10% step |
| AHM | Anterior–posterior heel-strike magnitude |
| AHS | Standard deviation of anterior-posterior acceleration during initial 10% step |
| ST | Step Time |
Top 10 selected features for peak COM excursion and MOS variability using LASSO, F-test, and ReliefF (* indicates that rank is the same each other).
| Rank | Peak COM Excursion | MOS Variability | ||||
|---|---|---|---|---|---|---|
| LASSO | F-Test | ReliefF | LASSO | F-Test | ReliefF | |
| 1 | vAHS | vAHS | sAHS | sLHS * | vAHS | sAHS |
| 2 | sLHS * | sAHS | aAHS | sAHS * | vLHM | sAMD |
| 3 | sAHS * | vAMD | aAM | sAMD * | vLM | aAMD |
| 4 | sST * | vAM | aAMD | aLHM * | vLMD | sLHS |
| 5 | sAMD | vLM | sAM | aAMD * | vLHS | sAM |
| 6 | aLHM | sVHM | sAMD | sVHM * | vST | vLM30 |
| 7 | aVHS | vLHM | aST | vLM30 | vAMD | vAHS |
| 8 | aVHM | vST | aAM30 | aVM30 | sVHM | aAM |
| 9 | aAMD | vLM30 | sLHS | vAHM | vVHM | sMD |
| 10 | sAM | sMD | vAHS | sMD | vAM | vM |
VIF values among top 10 features selected by each feature selection method for peak COM excursion and MOS variability (* indicates if VIF > 5).
| Feature | Peak COM Excursion | MOS Variability | ||||
|---|---|---|---|---|---|---|
| LASSO | F-Test | ReliefF | LASSO | F-Test | ReliefF | |
| 1 | 2.24 | 1.34 | 433.55 * | 1.61 | 4.12 | 7.12 * |
| 2 | 1.70 | 2.48 | 93.76 * | 1.53 | 12.88 * | 8.00 * |
| 3 | 2.11 | 1.38 | 164.77 * | 1.52 | 9.03 * | 3.66 |
| 4 | 1.94 | 6.71 * | 3.01 | 1.84 | 14.25 * | 2.88 |
| 5 | 3.01 | 9.51 * | 4.61 | 2.34 | 8.04 * | 2.48 |
| 6 | 2.33 | 8.57 * | 3.22 | 1.59 | 12.23 * | 1.48 |
| 7 | 1.54 | 1.69 | 2.14 | 2.22 | 14.18 * | 2.52 |
| 8 | 2.38 | 5.57 * | 1.50 | 1.63 | 9.11 * | 2.30 |
| 9 | 1.50 | 8.79 * | 2.35 | 1.62 | 8.02 * | 1.31 |
| 10 | 2.73 | 1.78 | 1.95 | 1.14 | 1.94 | 1.75 |
The names of the features for each model are shown in Table 3.
Comparison of prediction error (MAE) for each feature selection method in peak COM excursion and MOS variability.
| No. of | Peak COM Excursion | MOS Variability | ||||
|---|---|---|---|---|---|---|
| LASSO | F-Test | ReliefF | LASSO | F-Test | ReliefF | |
| 1 | 0.0997 | - | - | - | - | - |
| 2 | - | 0.0935 | 0.1007 | - | 0.0056 | 0.0061 |
| 3 | - | 0.0935 | 0.1006 | - | 0.0055 | 0.0051 |
| 4 | 0.0929 | 0.0936 | 0.1010 | - | 0.0056 | 0.0048 |
| 5 | 0.0916 | 0.0941 | 0.1007 | - | 0.0055 | 0.0049 |
| 6 | 0.0921 | 0.0947 | 0.0947 | 0.0045 | 0.0054 | 0.00474 |
| 7 |
| 0.0901 | 0.0946 | 0.0045 | 0.0054 |
|
| 8 | 0.0885 |
| 0.0960 | 0.0044 | 0.0052 | 0.00468 |
| 9 | 0.0885 | 0.0899 | 0.0945 | 0.0043 | 0.0052 | 0.00469 |
| 10 | 0.0890 | 0.0901 |
|
|
| 0.00472 |
The names of the features for each model are shown in Table 3.
Figure 2Scatter plots for predicted results vs. actual values: (a) peak COM excursion and (b) MOS variability.
Figure 3Comparison of the differences between actual values and predicted results for: (a) peak COM excursion and (b) MOS variability.
Results of the paired t-test and effect size between the actual and predicted values for peak COM excursion and MOS variability (* indicates p < 0.05).
| Dependent Variable | Group | Mean | Standard | Effect Size (Cohen’s | |
|---|---|---|---|---|---|
| Peak COM | Actual | 0.3585 | 0.1513 | 0.0527 | 0.0053 |
| Predicted | 0.3593 | 0.1041 | |||
| MOS | Actual | 0.0215 | 0.0090 | 0.0318 * | 0.0111 |
| Predicted | 0.0216 | 0.0078 |