Identification of Postural Controllers in Human Standing Balance

2020 ◽  
Vol 143 (4) ◽  
Author(s):  
Huawei Wang ◽  
Antonie J. van den Bogert

Abstract Standing balance is a simple motion task for healthy humans but the actions of the central nervous system (CNS) have not been described by generalized and sufficiently sophisticated control laws. While system identification approaches have been used to extracted models of the CNS, they either focus on short balance motions, leading to task-specific control laws, or assume that the standing balance system is linear. To obtain comprehensive control laws for human standing balance, complex balance motions, long duration tests, and nonlinear controller models are all needed. In this paper, we demonstrate that trajectory optimization with the direct collocation method can achieve these goals to identify complex CNS models for the human standing balance task. We first examined this identification method using synthetic motion data and showed that correct control parameters can be extracted. Then, six types of controllers, from simple linear to complex nonlinear, were identified from 100 s of motion data from randomly perturbed standing. Results showed that multiple time-delay paths and nonlinear properties are both needed in order to fully explain human feedback control of standing balance.

Sensors ◽  
2021 ◽  
Vol 21 (21) ◽  
pp. 7305
Author(s):  
Rachel V. Vitali ◽  
Vincent J. Barone ◽  
Jamie Ferris ◽  
Leia A. Stirling ◽  
Kathleen H. Sienko

This preliminary investigation studied the effects of concurrent and terminal visual feedback during a standing balance task on ankle co-contraction, which was accomplished via surface electromyography of an agonist–antagonist muscle pair (medial gastrocnemius and tibialis anterior muscles). Two complementary mathematical definitions of co-contraction indices captured changes in ankle muscle recruitment and modulation strategies. Nineteen healthy older adults received both feedback types in a randomized order. Following an analysis of co-contraction index reliability as a function of surface electromyography normalization technique, linear mixed-effects regression analyses revealed participants learned or utilized different ankle co-contraction recruitment (i.e., relative muscle pair activity magnitudes) and modulation (i.e., absolute muscle pair activity magnitudes) strategies depending on feedback type and following the cessation of feedback use. Ankle co-contraction modulation increased when concurrent feedback was used and significantly decreased when concurrent feedback was removed. Ankle co-contraction recruitment and modulation did not significantly change when terminal feedback was used or when it was removed. Neither ankle co-contraction recruitment nor modulation was significantly different when concurrent feedback was used compared to when terminal feedback was used. The changes in ankle co-contraction recruitment and modulation were significantly different when concurrent feedback was removed as compared to when terminal feedback was removed. Finally, this study found a significant interaction between feedback type, removal of feedback, and order of use of feedback type. These results have implications for the design of balance training technologies using visual feedback.


Author(s):  
Tuhin Das ◽  
Greg Semrau ◽  
Sigitas Rimkus

One of the key control problems associated with variable speed wind turbine systems is maximization of energy extraction when operating below the rated wind speed and power regulation when operating above the rated wind speed. In this paper, we approach these problems from a nonlinear systems perspective. For below rated wind speeds we adopt existing work appearing in the literature and provide further insight into the characteristics of the resulting equilibrium points of the closed-loop system. For above rated wind speeds, we propose a nonlinear controller and analyze the stability property of the resulting equilibria. We also propose a method for switching between the two operating regimes that ensures continuity of control input at the transition point. The control laws are verified using a wind turbine model with a standard turbulent wind speed profile that spans both operating regimes.


1999 ◽  
Vol 121 (2) ◽  
pp. 293-297 ◽  
Author(s):  
P. Gorce ◽  
M. Guihard

In this paper, we propose a general controller for complex tasks such as coordination or manipulation for grasping systems or dynamic gaits for legged robots. Moreover, this controller is adapted to pneumatic actuated structures. The aim is then to ensure a dynamic tracking of position and force for systems which may interact with the environment or cooperate with each other. For that, we propose a nonlinear controller based on a computed torque method taking into account the actuator and the mechanical models. The originality lays in the consideration of impedance behaviour at each joint during free and constrained tasks. It leads to continuous control laws between contact and non-contact phases. The asymptotic stability is ensured using Popov criteria. The application proposed is the control of one pneumatic leg of a biped robot. We present a dynamic model of the leg and chosen trajectories. Simulation results of this new controller are presented, leading to a good behaviour of the leg during a whole walking cycle at relatively high velocities.


2011 ◽  
Vol 212 (2) ◽  
pp. 279-291 ◽  
Author(s):  
David A. E. Bolton ◽  
William E. McIlroy ◽  
W. Richard Staines

2014 ◽  
Vol 8 (5) ◽  
pp. 204 ◽  
Author(s):  
Peng Yong-Tao ◽  
Wang Yue-Ping ◽  
Wei Wen-Ling ◽  
Wang Xiao-Ting

Unpowered drop test is very important for reusable launch vehicle (RLV) autolanding technology development. One of the challenges is to design an autolanding trajectory with enough robustness against uncertainties of drop conditions, aerodynamic characteristic and disturbances from control system and environment. In this paper, a   solution including trajectory generation and control design is proposed for a drop test RLV demonstrator. Firstly, the drop test and vertical flight trajectory are introduced. Also, parts of the drop flight, segments of landing trajecory and trajectory design parameters in groups are shown. Secondly, an online trajectory generation method including self-adapted capture segment plan and landing trajectory optimization following UAV auto-landing experience are illustrated in detail by designing groups of parameters. Then, simple but practical gain schedule control laws are presented. Finally, mathematic simulation and analysis based on both RSS and Monte Carlo methods indicate that the solution proposed has shown an acceptable robustness and can provide enough capability for the demonstrator to land saftly.


Author(s):  
Billy L. Luu ◽  
Thomas P. Huryn ◽  
H. F. Machiel Van der Loos ◽  
Elizabeth A. Croft ◽  
Jean-Sébastien Blouin

2012 ◽  
Vol 218 (1) ◽  
pp. 161-161
Author(s):  
David A. E. Bolton ◽  
William E. McIlroy ◽  
W. Richard Staines

Author(s):  
Gennadiy P. Аnshakov ◽  
◽  
Vadim V. Salmin ◽  
Alexey S. Chetverikov ◽  
Konstantin V. Peresypkin ◽  
...  

The article presents a formulation of a problem of trajectory optimization using low-thrust engines for an optical space system based on diffractive membranes. A methodology, where first stage nominal trajectories and control programs are selected and then corrected at the longrange guidance, has been developed for solving the problem of optimizing the trajectories of a flight to a geostationary orbit. At the final stage, algorithms for terminal control are formed, which allows to deliver a cosmic optical system based on diffraction membranes to a given point in the geostationary orbit. The end result is acquisition of Pareto-optimal solutions in the coordinates "characteristic speed-duration of the flight", where each point of the set of solutions has a corresponding a measure of accuracy of payload delivery to a geostationary orbit at a given set of coordinates.


2018 ◽  
Vol 24 (22) ◽  
pp. 5261-5272 ◽  
Author(s):  
Difan Tang ◽  
Lei Chen ◽  
Zhao F. Tian ◽  
Eric Hu

This paper proposes a novel adaptive nonlinear controller based on neural-networks (NNs) for active suppression of airfoil flutter (ASAF) from the optimal control perspective. Optimal control laws for locally nonlinear systems are synthesized in real time by solving the Hamilton–Jacobi–Bellman equation online with a proposed new form of NN-based value function approximation (VFA) and an extended Kalman filter. A systematic procedure based on linear matrix inequalities is further proposed for designing a scheduled parameter matrix that generalizes the new form of VFA to globally nonlinear systems to suit ASAF applications. Un-modeled dynamics are captured using an NN identifier. Comparisons drawn with a linear-parameter-varying optimal controller in wind-tunnel experiments confirm the effectiveness and validity of the proposed control scheme.


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