| Literature DB >> 32778127 |
M Bannwart1,2, S L Bayer3, N König Ignasiak4, M Bolliger3, G Rauter3,5,6, C A Easthope3,7.
Abstract
BACKGROUND: Body weight support systems with three or more degrees of freedom (3-DoF) are permissive and safe environments that provide unloading and allow unrestricted movement in any direction. This enables training of walking and balance control at an early stage in rehabilitation. Transparent systems generate a support force vector that is near vertical at all positions in the workspace to only minimally interfere with natural movement patterns. Patients with impaired balance, however, may benefit from additional mediolateral support that can be adjusted according to their capacity. An elegant solution for providing balance support might be by rendering viscous damping along the mediolateral axis via the software controller. Before use with patients, we evaluated if control-rendered mediolateral damping evokes the desired stability enhancement in able-bodied individuals.Entities:
Keywords: Balance; Body weight support; Gait; Mediolateral stability; Rehabilitation
Mesh:
Year: 2020 PMID: 32778127 PMCID: PMC7418206 DOI: 10.1186/s12984-020-00735-w
Source DB: PubMed Journal: J Neuroeng Rehabil ISSN: 1743-0003 Impact factor: 4.262
Fig. 1Experimental setup. a Subject walking with a harness and assistance from a 3-DoF, robotic BWS system (the FLOAT) on the treadmill. b List of used markers and their anatomical locations. C) Front and back view of pelvis marker placement next to BWS harness
Outcome parameters
| Name | Definition | Unit | Primary effect axis |
|---|---|---|---|
| Duty cycle | Percentage of stance phase over the whole cycle duration | % | anteroposterior |
| Step length | Anteroposterior distance between contralateral heel markers at their respective heel strikes plus the distance the stance foot moved back with the treadmill belt during this time | m | anteroposterior |
| Step width | Mediolateral distance between contralateral heel markers at their respective heel strikes | m | mediolateral |
| ML approximated COM (aCOM) sway | Difference between the ML extrema of the aCOM within each step | m | mediolateral |
| ML Margins of Stability (ML MoS) | Shortest distance of the floor-projected aCOM during midstance to the nearest edge of the base of support BoS was defined as the smallest convex hull spanning all points (heel, ankle, 5th metatarsal and 2nd metatarsal) in contact with the ground | m | mediolateral |
| Step width (CoV) | Standard deviation divided by the mean of step width | m | mediolateral |
| ML approximated COM (aCOM) sway (CoV) | Standard deviation divided by the mean of ML aCOM sway | m | mediolateral |
| ML λs pos | Short-term maximum Lyapunov exponent from time series of ML aCOM position | arbitrary unit | mediolateral |
| ML λs vel | Short-term maximum Lyapunov exponent from time series of ML aCOM velocity | arbitrary unit | mediolateral |
| VT λs pos | Short-term maximum Lyapunov exponent from time series of VT aCOM positions | arbitrary unit | vertical |
| VT λs vel | Short-term maximum Lyapunov exponent from time series of VT aCOM velocity | arbitrary unit | vertical |
Fig. 2Effects of damping on BWS end-effector motion. Line plots of estimated marginal means over the transparent and damped conditions for mediolateral and vertical BWS end-effector excursion. Plot includes error bars specifying 95%-confidence intervals (within-subject, [71]) and statistically significant differences denoted by p-values. Abbreviations: ML – mediolateral, VT – vertical
Repeated measures ANOVA test statistics for outcome parameters
| Parameter | F-statistic | |
|---|---|---|
| step length | F(1.41, 28.23) = 3.95) | |
| duty cycle | F(1.36, 27.21) = 37.88.15 | |
| step width | F(1.45, 29.06) = 4.73 | |
| ML aCOM sway | F(1.37, 27.46) = 65.93 | |
| ML MoS | F(1.55, 31.00) = 1.59 | |
| step width variability | F(1.41, 28.24) = 42.24 | |
| aCoM sway variability | F(1.40, 28.04) = 49.81 | |
| ML λs pos | F(2, 40) = 27.58 | |
| ML λs vel | F(2, 40) = 56.86 | |
| VT λs pos | F(1.43, 28.53) = 34.14 | |
| VT λs vel | F(1.45, 29.03) = 41.86 |
Fig. 3Effects of damped and undamped BWS on the anteroposterior and vertical axes. Line plots of estimated marginal means over the three stability conditions for outcomes related to the anteroposterior and vertical axes. Plot includes error bars specifying 95%-confidence intervals (within-subject, [71]) and statistically significant differences denoted by p-values. Abbreviations: VT – vertical, λs pos – short-term maximum Lyapunov exponent calculated from approximated center of mass position, λs vel – short-term maximum Lyapunov exponent calculated from approximated center of mass velocity
Fig. 4Effects of damped and undamped BWS on direct global dynamic stability. Line plots of estimated marginal means over the three stability conditions for outcomes reflecting direct global dynamic stability. Plot includes error bars specifying 95%-confidence intervals (within-subject, [71]) and statistically significant differences denoted by p-values. Abbreviations: ML – mediolateral, aCOM - approximated center of mass, MoS – Margins of stability
Fig. 5Effects of damped and undamped BWS on indirect global and local dynamic stability. Line plots of estimated marginal means over the three stability conditions for outcomes related to indirect global and local dynamic stability. Plot includes error bars specifying 95%-confidence intervals (within-subject, [71]) and statistically significant differences denoted by p-values. Abbreviations: ML – mediolateral, aCOM - approximated center of mass, CoV – coefficient of variance, λs pos – short-term maximum Lyapunov exponent calculated from approximated center of mass position, λs vel – short-term maximum Lyapunov exponent calculated from approximated center of mass velocity