Design and kinematic analysis of a Miura-oriented origami continuum space manipulator with deployable bending capability

Abstract. The capture of irregular, dimension-variable non-cooperative space debris remains a critical challenge for on-orbit servicing. This paper proposes a continuum gripper based on modified right-angle Miura-ori tessellation, integrating deployable folding and controllable large-range bending. Geometric relations of crease parameters are derived to build a parametric model mapping two-dimensional fold patterns to three-dimensional deployed configurations. An improved Denavit–Hartenberg (D–H) method provides closed-form kinematic solutions, with workspace evaluated via Monte Carlo simulation. A tendon-driven three-finger prototype is tested. Kinematic experiments verify position prediction accuracy and workspace positioning capability. Grasping tests on typical debris simulants confirm passive adaptation and stable enclosure. Load experiments achieve a 265.8 g payload and 100 % grasping success rate, validating the mechanism's controllability and adaptability for on-orbit grasping applications.

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Publication Details

Journal
Mechanical sciences
Published
2026-05-29
DOI
https://doi.org/10.5194/ms-17-645-2026
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
0.00

Funders

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article

Design and kinematic analysis of a Miura-oriented origami continuum space manipulator with deployable bending capability

Manjia Su, Ruiwei Liu, Jinhui Zhou, Kengyi Wang et al.
Mechanical sciences
Space Satellite Systems and Control
article

Design and kinematic analysis of a Miura-oriented origami continuum space manipulator with deployable bending capability

Manjia Su, Ruiwei Liu, Jinhui Zhou, Kengyi Wang, Haoyu Yang, Hongwei Guo, Mengyu Zhong, Chunlong Wang
article en

Abstract

Abstract. The capture of irregular, dimension-variable non-cooperative space debris remains a critical challenge for on-orbit servicing. This paper proposes a continuum gripper based on modified right-angle Miura-ori tessellation, integrating deployable folding and controllable large-range bending. Geometric relations of crease parameters are derived to build a parametric model mapping two-dimensional fold patterns to three-dimensional deployed configurations. An improved Denavit–Hartenberg (D–H) method provides closed-form kinematic solutions, with workspace evaluated via Monte Carlo simulation. A tendon-driven three-finger prototype is tested. Kinematic experiments verify position prediction accuracy and workspace positioning capability. Grasping tests on typical debris simulants confirm passive adaptation and stable enclosure. Load experiments achieve a 265.8 g payload and 100 % grasping success rate, validating the mechanism's controllability and adaptability for on-orbit grasping applications.

Mechanical sciencesVol. 17(1)
National Natural Science Foundation of China
Openalex Percentile: Top 2%
Space Satellite Systems and Control
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