Directional singularity-robust torque control for gyroscopic actuators

Journal Article (2016)
Author(s)

Andrew Berry (TU Delft - OLD Biorobotics)

D.S. Lemus Perez (TU Delft - OLD Biorobotics)

R. Babuska (TU Delft - OLD Intelligent Control & Robotics)

H. Vallery (TU Delft - OLD Biorobotics)

Research Group
OLD Biorobotics
Copyright
© 2016 Andrew Berry, D.S. Lemus Perez, R. Babuska, H. Vallery
DOI related publication
https://doi.org/10.1109/TMECH.2016.2603601
More Info
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Publication Year
2016
Language
English
Copyright
© 2016 Andrew Berry, D.S. Lemus Perez, R. Babuska, H. Vallery
Research Group
OLD Biorobotics
Issue number
6
Volume number
21
Pages (from-to)
2755 - 2763
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Abstract

Gyroscopic actuation is appealing for wearable applications due to its ability to impart free moments on a body without exoskeletal structures on the joints.We recently proposed an unobtrusive balancing aid consisting of multiple parallelmounted control moment gyroscopes (CMGs) contained within a backpack-like orthopedic corset. Using conventional CMG control techniques, geometric singularities result in a number of performance issues, including either unintended oscillations or freezing of the gimbals at certain alignments, which are typically mitigated by the addition of redundant actuators or by allowing errors in the generated moment; however, because of the minimalistic design of the proposed device and focus on accurate moment tracking, a new methodology is required. In this paper, a control scheme is proposed for non-redundant CMG systems in which oscillations at saturated states are avoided and all remaining singularities are efficiently escaped by exploiting the system geometry; due to its use of classification-specific singularity proximity measures that account for the command moment orientation, it is named the directional singularity-robust (DSR) control law. The performance of this control law is assessed in both simulations and hardware testing. The proposed method is suitable for a wide range of CMG systems, including both balancing and aerospace applications.

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