Abstract
Metamaterials with multimodal deformation mechanisms resemble machines1,2, especially when endowed with autonomous functionality. A representative architected assembly, with tunable chirality, converts linear motion into rotation3. These chiral metamaterials with a machine-like dual modality have potential use in areas such as wave manipulation4, optical activity related to circular polarization5 and chiral active fluids6. However, the dual motions are essentially coupled and cannot be independently controlled. Moreover, they are restricted to small deformation, that is, strain ≤2%, which limits their applications. Here we establish modular chiral metamaterials, consisting of auxetic planar tessellations and origami-inspired columnar arrays, with decoupled actuation. Under single-degree-of-freedom actuation, the assembly twists between 0° and 90°, contracts in-plane up to 25% and shrinks out-of-plane more than 50%. Using experiments and simulations, we show that the deformation of the assembly involves in-plane twist and contraction dominated by the rotating-square tessellations and out-of-plane shrinkage dominated by the tubular Kresling origami arrays. Moreover, we demonstrate two distinct actuation conditions: twist with free translation and linear displacement with free rotation. Our metamaterial is built on a highly modular assembly, which enables reprogrammable instability, local chirality control, tunable loading capacity and scalability. Our concept provides routes towards multimodal, multistable and reprogrammable machines, with applications in robotic transformers, thermoregulation, mechanical memories in hysteresis loops, non-commutative state transition and plug-and-play functional assemblies for energy absorption and information encryption.
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Data availability
The experimental data supporting the findings of this study are openly available at Zenodo56 (https://doi.org/10.5281/zenodo.14676200). Source data are provided with this paper.
Code availability
The simulation codes supporting the findings of this study are openly available at Zenodo56 (https://doi.org/10.5281/zenodo.14676200).
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Acknowledgements
We thank B. Kresling (creator of the Kresling pattern), E.A. Paulino, S. Kahn, T. Tachi, C.M. Sharpless, J. Russ, L. Novelino and K.T. Liu for their discussions; P.T. Brun for assistance with the mechanical testing of the reprogrammable assembly; and Y. Rao for her comments and suggestions on the manuscript. This research was supported by Margareta E. Augustine Professorship of Engineering at Princeton University and the National Science Foundation under grant no. 2323276. We also acknowledge support from the Andlinger Center for Energy and the Environment, the Princeton Materials Institute, and the Council on Science and Technology at Princeton University.
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Contributions
T.Z. and G.H.P. proposed and developed the research idea. T.Z. designed and fabricated the Kresling origami samples and tessellations. T.Z. and X.D. conceptualized the actuation of the origami assemblies. X.D. developed the computational framework, performed simulations, analysed the data and provided the Preisach model. T.Z. and S.Z. performed mechanical testing of the Kresling origami assemblies. K.M. and M.C. designed the magnetic drive hardware and software and T.Z. and K.M. performed the magnetic experiments. J.M. and G.H.P. originated the thermoregulation concept and T.Z. and S.Z. designed it. X.D. and S.Z. implemented non-commutative state transition experiments. G.H.P. supervised the project. All co-authors provided feedback and contributed to the paper.
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Extended data figures and tables
Extended Data Fig. 1 Modular lattice cell geometry.
a, From standard shell-based origami to the rod-based lattice unit. Visual comparison between a paper-folded Kresling origami (left) and a 3D-printed lattice prototype (right). The diameter of the rods is 1.5 mm (scale bar, 5 mm). b, Schematic of a 6-gon unit in the deployed state (left) and in the folded state (middle). The top view (right) of the unit highlights two twist angles, φ1 and φ0, which define the position of the top polygon in the two stable states. h1, deployed unit height; h0, folded unit height; u, displacement; c, valley rod length; b, mountain rod length; r, polygon radius. c, The strain energy of the unit versus twist angle obtained with the bar-and-hinge method. d, The height of the unit versus twist angle.
Extended Data Fig. 2 Schematics of mechanical test setups: boundary conditions and loading conditions.
a, Axial translation fixture for standard tests with displacement control. Left and right: for results in left and right of Fig. 6e, respectively. Middle: for Fig. 5. b, Dedicated fixture for rotational test with free translation57. This fixture is used for obtaining results in Figs. 2, 6d, Extended Data Fig. 8, and Supplementary Fig. S4. c, Alternative fixtures for linear displacement with free rotation. Left: Supplementary Fig. S5. Middle: Supplementary Fig. S6. Right: Fig. 3 and Supplementary Fig. S7.
Extended Data Fig. 3 Surrogate model simulation for multimodal deformations of the chiral modular cells.
a, The modular cells (frames) and the origami models (shells). b, Mechanical springs in the surrogate model. c, Torque-twist-angle curves from the twisting simulation of three cells of the same geometry but different material properties. d, Force-displacement curves from the compression simulation of three cells of the same geometry but different material properties.
Extended Data Fig. 4 Surrogate model simulation for multimodal deformations of the chiral modular columns with different constituent cells.
a, Torque versus cumulative twist angle from the twisting simulation of the columns. b, Deformation snapshots of the twisted columns. The two boxes indicate the configurations with corresponding experimental results (Extended Data Fig. 5). c, Force versus displacement from the compression simulation of the columns. d, Deformation snapshots of the compressed columns.
Extended Data Fig. 5 Twisting experiments of two columns that differ by their chiral modular arrangement and material composition.
a, Surrogate model simulations. b, Experimental results. c, Snapshots illustrating the twisting experiment with free translation. d, Experimental results of torque versus cumulative twist angle.
Extended Data Fig. 6 Electrical system for the precise control of the magnetically actuated robotic metamaterial.
a, Experimental setup consisting of a dc power source, a scalable power converter, and a set of copper coils. b, Modular power converter prototype comprising six individual power electronic building blocks. c, 3-D Helmholtz coil structure made of six circular-winding pairs; each pair consists of two windings connected in series. d, Scalable power-converter topology consisting of six full-bridge submodules to precisely control the current of each winding pair. e, System block diagram showing the closed loop current-control scheme; the winding currents are sensed locally in each submodule using shunt resistors. A proportional-integral controller is implemented on a microcontroller card resulting in an equivalent first order reference-to-winding current system. Each coil is modeled by an inductance value L and a resistance R representing the resistivity of the copper wire. The controller gains are selected as \({k}_{p}=L/{t}_{r}ln9\) and \({k}_{i}=R/{t}_{r}ln9\) to accomplish a 10% to 90% current rise time of tr = 1.5 ms. A pulse width modulator (PWM) employing a 10 kHz triangular carrier wave is used to generate the signals controlling the states of the individual power switches.
Extended Data Fig. 7 The optically augmented multistable origami assembly.
a, Digital image of the prototype in the deployed state. b, Prototype in the folded state. c, Interactive algorithm for parametric modelling with calculation of the origami cell in the deployed state. d, Interactive algorithm for parametric modelling with calculation of the origami cell in the folded state.
Extended Data Fig. 8 Non-commutative state transition of the two-layer chiral metamaterial.
a, The possible states of the metamaterial. A two-bit number is used to indicate the global states, with each bit representing an entire layer. For each bit, the digit 1 indicates that the layer is deployed, and the digit 0 indicates that the layer is folded. b–e, Experimental loading curves for state transitions (b) starting from 11 with a anticlockwise rotation followed by a clockwise rotation, (c) starting from 11 with a clockwise rotation followed by a anticlockwise rotation, (d) starting from 00 with a clockwise rotation followed by a anticlockwise rotation, (e) starting from 00 with a anticlockwise rotation followed by a clockwise rotation. The peak torques that trigger the state transitions are indicated in the plots.
Supplementary information
Supplementary Information (download PDF )
This file contains Supplementary Figs. 1–18, Supplementary Table 1 and additional references.
Supplementary Video 1 (download MP4 )
Twist experiment.
Supplementary Video 2 (download MP4 )
Linear displacement experiment.
Supplementary Video 3 (download MP4 )
Multimodal metamaterial simulations.
Supplementary Video 4 (download MP4 )
Plug-and-play: reconfigurable assemblies.
Supplementary Video 5 (download MP4 )
Magnetic robot transformer.
Supplementary Video 6 (download MP4 )
Non-commutative state transition.
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Zhao, T., Dang, X., Manos, K. et al. Modular chiral origami metamaterials. Nature 640, 931–940 (2025). https://doi.org/10.1038/s41586-025-08851-0
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DOI: https://doi.org/10.1038/s41586-025-08851-0
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