Conference paper
Origami-inspired deployable structures for space exploration: Integrating artificial intelligence, robotics, and advanced materials
IAF Materials and Structures Symposium - Held at the 76th International Astronautical Congress, IAC 2025, pp 601-614
2025
Abstract
Next-generation space exploration requires deployable structures that are lightweight, compact, and resilient under harsh orbital and planetary conditions. This paper proposes a conceptual framework for origami-inspired deployable systems, merging insights from Artificial Intelligence (AI), Robotics, and advanced materials research. By incorporating folding techniques such as Miura-ori and Yoshimura tessellations, this approach aims to significantly reduce stowage volume and mass while preserving structural integrity during deployment. Central to this framework is finite element analysis (FEA), used to investigate stress distribution, deformation, and dynamic responses under launch vibrations, microgravity, and extreme temperature fluctuations. Carbon fiber-reinforced polymers and shape-memory alloys (SMAs) serve as primary materials, chosen for their superior strength-to-weight ratios, adaptability, and radiation resistance. An evolutionary generative design methodology—employing multi-objective genetic algorithms with parametric constraints for mechanical properties and fold patterns—optimizes deployment strategies by iteratively balancing mass efficiency, rigidity, and reliability. The system also integrates robotic platforms equipped with precision actuators, sensors, and kinematic models rooted in rigid body and multi-body dynamics. These autonomous robots govern real-time folding and unfolding operations, adapting to anomalies such as unexpected oscillations or partial misalignments. Structural health monitoring is achieved using embedded sensor networks, including fiber-optic arrays, which enable continuous measurements of stress, strain, and temperature. Advanced analytics—covering predictive maintenance algorithms and anomaly detection—preempt potential material fatigue or mechanical failures, thereby minimizing downtime and extending operational lifespans. Methodologically, nonlinear dynamics, control theory, and multi-objective optimization form the theoretical underpinning, ensuring robust performance under evolving mission constraints. Scaled prototypes will be tested in vacuum chambers, radiation test beds, and wide temperature extremes to validate overall feasibility. Expected outcomes include higher deployment accuracy, reduced mass budgets, and improved reusability compared to conventional deployable systems. Future research will delve into electroactive polymers, 4D printing, and the scaling of these origami-inspired designs for large-scale applications, from space habitats to expansive solar sails. By fusing origami engineering, robotic autonomy, and innovative material science, this framework offers a pioneering avenue for developing adaptable, resilient, and highly efficient space structures.
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Details
- Title
- Origami-inspired deployable structures for space exploration: Integrating artificial intelligence, robotics, and advanced materials
- Creators
- Nijanthan Vasudevan - Department of Mechanical, Materials & Aerospace Engineering, West Virginia University, Morgantown, WV, United StatesOudayl MassatArjuna Karthikeyan Senthilvel Kavitha - Drexel University, College of EngineeringPadmapriya Sampathkumar
- Publication Details
- IAF Materials and Structures Symposium - Held at the 76th International Astronautical Congress, IAC 2025, pp 601-614
- Conference
- IAF Materials and Structures Symposium (Sydney, Australia, 29 Sep 2025–03 Oct 2025)
- Publisher
- International Astronautical Federation (IAF)
- Number of pages
- 14
- Resource Type
- Conference paper
- Language
- English
- Academic Unit
- College of Engineering
- Scopus ID
- 2-s2.0-105036202770
- Other Identifier
- 991022182368604721