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ORIGINAL RESEARCH article

Front. Space Technol.
Sec. Space Robotics
Volume 5 - 2024 | doi: 10.3389/frspt.2024.1447545
This article is part of the Research Topic Vibration Control of Space Manipulators: Advances and Challenges View all articles

Tip and Vibration Control of Space Robots Using Estimated Flexible Coordinates

Provisionally accepted
  • Institute for Aerospace Studies, Faculty of Applied Science & Engineering, University of Toronto, Toronto, Canada

The final, formatted version of the article will be published soon.

    This paper provides an extension to previous work on end-effector control of flexible space manipulators. Those works considered the use of a special output called the µ-tip rate for feedback control of desired end-effector trajectories with simultaneous vibration control. Implementation of this special output requires measurement of end-effector position or the use of flexible forward kinematics to determine it. For the latter, one requires measurements of the joint angles and flexible coordinates. The second of these is difficult to measure in space scenarios, so this paper looks at the use of an estimation scheme to approximate it and use it in a task-space control law. Multiple simulations are conducted to investigate the use of these approximated elastic coordinates in robustly controlling a one-link and two-link flexible manipulator with a payload mass.The error between desired and actual trajectory is calculated, and the results are juxtaposed with results from a joint-space feedback scheme. There is an emphasis on comparing the estimated elastic coordinates with the actual simulated coordinates. Using the estimated elastic coordinates to determine the end-effector location via forward kinematics, yielded similar results to when the actual elastic coordinates were used. Overall, the estimation equation used is shown to provide reasonable end-effector tracking results with the end-effector being able to track various types of trajectories.

    Keywords: Flexible space manipulators, Vibration suppression, flexible coordinate estimation, task-space control, Tip Control

    Received: 11 Jun 2024; Accepted: 03 Sep 2024.

    Copyright: © 2024 Patel and Damaren. This is an open-access article distributed under the terms of the Creative Commons Attribution License (CC BY). The use, distribution or reproduction in other forums is permitted, provided the original author(s) or licensor are credited and that the original publication in this journal is cited, in accordance with accepted academic practice. No use, distribution or reproduction is permitted which does not comply with these terms.

    * Correspondence: Christopher J. Damaren, Institute for Aerospace Studies, Faculty of Applied Science & Engineering, University of Toronto, Toronto, Canada

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