Combining Inertial Sensors and Machine Learning to Predict vGRF and Knee Biomechanics during a Double Limb Jump Landing Task
<p>Overview of project. For the calculation of laboratory-based biomechanics, we collected motion-capture and force plates data. We used inverse kinematics and inverse dynamics to calculate vGRF (peak vertical ground reaction force), KFA (peak knee flexion angle), KEM (peak knee extension moment), and KPA (peak sagittal plane knee power absorption). For the modeling of inertial measurement unit (IMU)-based biomechanics, we collected IMU data concurrently. We then selected the region of interest of these time series and extracted features (feature engineering). Next, we developed algorithms to predict the lab-based biomechanics. We evaluated the error of the IMU-based biomechanics against the lab-based biomechanics.</p> "> Figure 2
<p>Pictures of marker and IMU configurations. (<b>a</b>) IMU placement; (<b>b</b>) Frontal view of full marker configuration; (<b>c</b>) Sagittal view of full marker configuration.</p> "> Figure 3
<p>Description of task and steps to select region of interest (ROI)-based on IMUs. (<b>A</b>) Task. Participants jumped forward from a 30 cm tall box to side-by-side force plates positioned ½ body height forward in distance. Immediately upon landing, they completed a maximum vertical jump and landed back on the force plates. The region of interest to extract biomechanical variables was from initial contact of the first landing until maximum knee flexion during that landing. (<b>B</b>) Step 1. Identification of the initial ROI based on the 2 most prominent local minima of the resultant thigh acceleration after applying a 1.5 Hz low-pass filter. Circles indicate these two points. (<b>C</b>). Step 2, “Start.” Identification of the “start” within the ROI from step 1, based on the local minimum immediately preceding when the high-g shank x signal crossed 20 g’s. A black circle indicates this point. (<b>D</b>). Step 3, “Stop.” Identification of the end of the ROI when the thigh gyroscope data was greater than 0 for at least 50 frames. A red circle indicates this point. vGRF and knee flexion angles are overlaid to show that the ROI targeted the first half of the landing, from approximate initial contact to maximum knee flexion angle. IMUs, inertial measurement units. ROI, region of interest. vGRF, peak vertical ground reaction force. KFA, peak knee flexion angle. KEM, peak internal knee extension moment. KPA, peak sagittal plane knee power absorption. BW, body weight. HT, height.</p> "> Figure 4
<p>Scatter plots of expected (based on motion capture and force plates) vs. predicted (based on IMUs) values for each model by response variable. Each dot represents a limb-trial. Dots are colored according to the average nRMSE (normalized root mean square error) of the model, meaning darker colored models had a higher percent of normalized error, while lighter colored models had a lower percent of normalized error. vGRF, peak vertical ground reaction force. KFA, peak knee flexion angle. KEM, peak internal knee extension moment. KPA, peak sagittal plane knee power absorption. BW, body weight. HT, height.</p> "> Figure A1
<p>Scatter plots of expected (based on motion capture and force plates) vs. predicted (based on IMUs) limb symmetry index (LSI) values for each model by response variable. Each dot represents a limb-trial. Dots are colored according to the average RMSE (root mean square error) of the model, meaning darker colored models had higher error, while lighter colored models had a lower error. vGRF, peak vertical ground reaction force. KFA, peak knee flexion angle. KEM, peak internal knee extension moment. KPA, peak sagittal plane knee power absorption.</p> ">
Abstract
:1. Introduction
2. Materials and Methods
2.1. Overview
2.2. Participants
2.3. Data Collection
2.4. Laboratory-Based Biomechanical Analysis (Motion Capture and Force Plates)
2.5. Inertial Measurement Unit (IMU)-Based Biomechanical Analysis
2.5.1. Region of Interest
- We corrected all right limb IMUs to mirror the axes of the left limb IMUs. We applied a second-order, 1.5 Hz low-pass Butterworth filter [36] on the thigh high-g accelerometer time-series for all three axes and then calculated the resultant acceleration. We found the two most prominent [37] local minima of the resultant acceleration and defined the initial ROI as the region between these two points. An example trial can be seen in Figure 3B.
- To further refine the ROI, we used the selected region from step one, then determined “start” and “end” points within this region. Since optimal filtering parameters of inertial sensors during landing tasks have not been established, we explored a range of low pass filtering parameters from 15 Hz [28] up to unfiltered. Ultimately, we elected to apply a second-order, 50 Hz low-pass Butterworth filter on all IMU time-series data. This filter allowed for reliable feature extraction while visually appearing to reduce high frequency noise. The start point occurred at the local minimum directly preceding when the shank x (aligned axially on the shank) high-g accelerometer first exceeded 20 g’s for five consecutive frames (4 ms). The end point occurred after the start point, when the thigh z (aligned with the medial-lateral axis of the thigh) gyroscope exceeded 0 rad/sec for at least 50 frames (40 ms) forward, indicating angular velocity of the thigh towards relative extension. All trials were visually inspected with overlaid vGRF and KFA to ensure these steps yielded an appropriate region. A visualization of these steps for a representative limb-trial is shown in Figure 3C,D.
2.5.2. Feature Engineering
2.5.3. Algorithm Development
2.5.4. Algorithm Evaluation
3. Results
4. Discussion
4.1. Overview of Findings
4.2. Absolute vs. Relative Measures of Biomechanical Variables
4.3. Comparing and Contrasting Double and Single Limb Landings
4.4. Benefits and Drawbacks of Single-Feature vs. Multiple-Feature Solutions
- We recommend that the use of single features is ideally suited for feedback interventions, and we advocate for future interventional research to demonstrate the effectiveness of manipulating knee-specific biomechanics post-ACLR.
- We recommend the use of multiple feature models for improved fidelity in objectively assessing biomechanics during landing tasks outside a laboratory setting.
4.5. Machine Learning Approaches
4.6. Variability of Landing Strategy
4.7. Additional Considerations
5. Conclusions
Author Contributions
Funding
Institutional Review Board Statement
Informed Consent Statement
Data Availability Statement
Acknowledgments
Conflicts of Interest
Appendix A
Feature Name | Abbreviation |
---|---|
Max | max |
Time to max | ttmax |
Max prominence | pmax |
Width of max | wmax |
Min | min |
Time to min | ttmin |
Min prominence 1 | pmin |
Width of min | wmin |
Max-min difference | mmdiff |
Max-min time difference | mmtdiff |
Start value | start |
Stop value | stop |
Standard deviation | std |
Area under the curve | auc |
Response | Shank | Thigh |
---|---|---|
vGRF | Accel R: std | Accel R: std |
KFA | Accel Z: std | Gyro Z: auc |
KEM | Accel X: std | Accel Y: std |
KPA | Accel X: std | Accel Y: std |
Response | Shank Accel | Thigh Accel | Other |
---|---|---|---|
vGRF | X: start, auc Y: max, pmax Z: wmax, min R: stop, std, auc | X: auc Y: start, ttmax, pmin, auc Z: start, pmax, wmin, auc R: start, stop, mmdiff | |
KFA | X: start, std, min, pmin, mmtdiff, auc Y: start Z: std, ttmin, mmdiff R: start, stop | X: wmin, auc Y: min, wmin, auc Z: start, pmin, mmdiff R: auc | Range |
KEM | X: start, ttmax Z: start, w max R: std, max, ttmax, min | X: std, wmax, mmdiff, auc Y: start, wmax, auc Z: wmax, pmax, mmdiff, mmtdiff, auc R: start, ttmax, wmin, auc | |
KPA | X: min, ttmin, pmin, mmtdiff Y: ttmax, wmin, auc Z: wmax, pmax, mmtdiff R: std, max, wmax | X: auc Y: start, std, max, pmax, pmin Z: start, std, ttmax, pmax, wmin, auc R: start, wmax, pmax, ttmin, pmin |
Shank | Thigh | ||||
---|---|---|---|---|---|
Response | Accel | Gyro | Accel | Gyro | Other |
vGRF | X: start, ttmin, auc Y: std, min R: start, std, ttmax | Y: start, std, pmax, ttmin Z: ttmin R: start, max, pmax | Y: pmin Z: wmin, pmin, auc R: stop | X: ttmax, wmax Y: mmdiff, auc Z: auc R: start | |
KFA | X: std, mmdiff, mmtdiff, auc Y: mmtdiff Z: ttmax R: start, stop | X: wmax, pmax, auc Y: std, wmax R: start, std, min | X: std, mmdiff Y: start, pmax, auc Z: start, std, auc R: wmax, auc | X: std, ttmax, auc Y: start, auc Z: start, std, wmax, pmax, pmin, auc R: start, mmtdiff | Range |
KEM | X: std Y: ttmax Z: start, mmdiff R: std, ttmax, pmax, min | X: wmax Z: std, min R: start, ttmax | X: wmax, pmax, auc Y: start, wmax, auc Z: mmdiff R: ttmax, wmax, wmin | X: std, max Z: std, mmdiff R: ttmax, wmax, wmin, pmin | |
KPA | X: std, ttmax Y: wmin Z: wmax, ttmin, pmin, mmdiff R: std, pmax | X: min Z: stop, std R: start | X: ttmax, auc Y: start, std, max, pmax Z: std, ttmax, pmax, wmin, pmin R: start, ttmax, ttmin, pmin | X: std, mmdiff Y: std Z: max, wmax |
Appendix B
Model RMSE (%) | |||||
---|---|---|---|---|---|
LSI (%) | Single Feature | Multiple Feature | |||
Mean ± SD | Shank | Thigh | Accel | Accel + Gyro | |
vGRF | 89.8 ± 19.5 | 15.2 | 17.9 | 14.7 | 14.3 |
KFA | 102.2 ± 4.1 | 4.1 | 4.2 | 4.0 | 3.5 |
KEM | 92.4 ± 16.8 | 15.8 | 16.3 | 13.9 | 12.7 |
KPA | 92.3 ± 23.2 | 21.9 | 20.2 | 17.0 | 15.8 |
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Category | Variable Name | Calculation |
---|---|---|
Max | Max | Maximum value |
Time to max | Frame number at maximum value | |
Max prominence 1 | Height of maximum relative to surrounding time-series | |
Width of max | Width (number of frames) at half-prominence 1 | |
Min | Min | Minimum value |
Time to min | Frame number at minimum value | |
Min prominence 1 | Height of minimum relative to surrounding time-series | |
Width of min | Width (number of frames) at half-prominence 1 | |
Max-min | Max-min difference | Maximum value–minimum value |
Max-min time difference | Time to max–time to min | |
Other | Start value | Value at start of ROI |
Stop value | Value at end of ROI | |
Standard deviation | Standard deviation of all elements | |
Area under the curve | Approximate integral using trapezoidal numerical integration |
Model | |||||
---|---|---|---|---|---|
Single Feature | Multiple Feature | ||||
Shank | Thigh | Accel | Accel + Gyro | ||
Model input parameters | Sensor location(s) | Shank | Thigh | Shank and thigh | |
Signals | Accel, gyro | Accel | Accel, gyro | ||
Potential features | 113 | 113 | 113 | 225 | |
Model training and selection | Model used | Simple linear regression | Stepwise linear regression | ||
Hyperparameter optimization | No | Yes | |||
# of selected features | 1 | Up to 41 | |||
Model selection | Highest R2 | High R2, low # of features | |||
Cross-validation | No | Yes, k-fold, n = 10 | |||
Performance evaluation | Goodness of fit | R2 | R2 | ||
Error | RMSE, nRMSE | RMSE, nRMSE |
Variable | N | Mean ± SD | Range [Min, Max] | Mean within- Participant SD | Mean between-Participant SD |
---|---|---|---|---|---|
vGRF (xBW) | 416 | 2.07 ± 0.57 | [0.96, 4.63] | 0.32 | 0.48 |
KFA (deg) | 416 | 93.9 ± 14.4 | [58.9, 136.9] | 5.0 | 13.8 |
KEM (xBW xHT) | 416 | 0.262 ± 0.046 | [0.138, 0.402] | 0.033 | 0.031 |
KPA (xBW xHT) | 413 | 2.01 ± 0.48 | [0.87, 3.72] | 0.33 | 0.38 |
Model | Cross-Validation | ||||||
---|---|---|---|---|---|---|---|
Single Feature | Multiple Feature | Multiple Feature | |||||
Shank | Thigh | Accel | Accel + Gyro | Accel | Accel + Gyro | ||
vGRF (xBW) | Features (#) | 1 | 1 | 21 | 27 | ||
R2 | 0.58 | 0.36 | 0.82 * | 0.87 * | 0.78 ± 0.01 | 0.83 ± 0.01 | |
RMSE | 0.37 | 0.46 | 0.24 | 0.21 | 0.25 ± 0.003 | 0.22 ± 0.002 | |
nRMSE (%) | 10.0 | 12.5 | 6.5 | 5.7 | 6.8 + 0.08 | 6.0 ± 0.05 | |
KFA (deg) | Features (#) | 1 | 1 | 23 | 41 | ||
R2 | 0.24 | 0.60 | 0.83 * | 0.94 * | 0.80 ± 0.01 | 0.92 ± 0.003 | |
RMSE | 12.6 | 9.1 | 6.1 | 3.6 | 6.2 ± 0.05 | 3.8 ± 0.04 | |
nRMSE (%) | 16.2 | 11.7 | 7.8 | 4.6 | 7.9 ± 0.06 | 4.9 ± 0.05 | |
KEM (xBW xHT) | Features (#) | 1 | 1 | 24 | 31 | ||
R2 | 0.17 | 0.16 | 0.59 | 0.68 | 0.50 ± 0.01 | 0.60 ± 0.01 | |
RMSE | 0.042 | 0.042 | 0.030 | 0.027 | 0.031 ± 0.0002 | 0.028 ± 0.0002 | |
nRMSE (%) | 15.9 | 15.9 | 11.4 | 10.2 | 11.7 ± 0.07 | 10.6 ± 0.07 | |
KPA (xBW xHT) | Features (#) | 1 | 1 | 30 | 33 | ||
R2 | 0.27 | 0.34 | 0.63 | 0.72 | 0.53 ± 0.02 | 0.64 ± 0.01 | |
RMSE | 0.41 | 0.39 | 0.30 | 0.26 | 0.32 ± 0.003 | 0.27 ± 0.003 | |
nRMSE (%) | 14.3 | 13.7 | 10.5 | 9.1 | 11.2 ± 0.1 | 9.5 ± 0.1 |
Prior Research | Current Models (RMSE) | |||||||
---|---|---|---|---|---|---|---|---|
Single Feature | Multiple Feature | |||||||
Variable | Reference | ACLR Involved | Healthy Control | Diff. | Shank | Thigh | Accel | Accel + Gyro |
vGRF | Paterno et al. [41] | 1.77 | 2.01 | 0.24 | 0.37 | 0.46 | 0.24 | 0.21 |
KFA | Delahunt et al. [42] | 62.0 | 69.5 | 7.5 | 12.6 | 9.1 | 6.1 | 3.6 |
KEM | Goerger et al. [43] | 0.169 | 0.204 | 0.035 | 0.042 | 0.042 | 0.030 | 0.027 |
KPA | White et al. [40] | 1.65 | 2.01 | 0.36 | 0.41 | 0.39 | 0.30 | 0.26 |
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Chaaban, C.R.; Berry, N.T.; Armitano-Lago, C.; Kiefer, A.W.; Mazzoleni, M.J.; Padua, D.A. Combining Inertial Sensors and Machine Learning to Predict vGRF and Knee Biomechanics during a Double Limb Jump Landing Task. Sensors 2021, 21, 4383. https://doi.org/10.3390/s21134383
Chaaban CR, Berry NT, Armitano-Lago C, Kiefer AW, Mazzoleni MJ, Padua DA. Combining Inertial Sensors and Machine Learning to Predict vGRF and Knee Biomechanics during a Double Limb Jump Landing Task. Sensors. 2021; 21(13):4383. https://doi.org/10.3390/s21134383
Chicago/Turabian StyleChaaban, Courtney R., Nathaniel T. Berry, Cortney Armitano-Lago, Adam W. Kiefer, Michael J. Mazzoleni, and Darin A. Padua. 2021. "Combining Inertial Sensors and Machine Learning to Predict vGRF and Knee Biomechanics during a Double Limb Jump Landing Task" Sensors 21, no. 13: 4383. https://doi.org/10.3390/s21134383
APA StyleChaaban, C. R., Berry, N. T., Armitano-Lago, C., Kiefer, A. W., Mazzoleni, M. J., & Padua, D. A. (2021). Combining Inertial Sensors and Machine Learning to Predict vGRF and Knee Biomechanics during a Double Limb Jump Landing Task. Sensors, 21(13), 4383. https://doi.org/10.3390/s21134383