Innovative Modular Design and Kinematic Approach based on Screw Theory for Triple Scissors Links Deployable Space Antenna Mechanism Article Swipe
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· 2025
· Open Access
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This paper presents the geometry design and analysis of a novel triple scissors links deployable antenna mechanism (TSDAM) to deal with the problems of large aperture and high precision space antennas for deep space communication and Earth observation. This mechanism has only one degree of freedom (DoF) and thus makes for efficient and reliable deployment without loss of structural integrity. It employed a systematic design approach starting from a triple scissors links modular unit to a 25m aperture assembly. Different configurations constituting variable numbers of modular units were analyzed in SolidWorks to identify the deployable mechanism with lowest deformation. While the 24 units configuration offered superior stowage compactness, it exhibited higher deformation (0.01437mm), confirming the 12 units configuration as the optimal balance between structural stability and deployment efficiency. Screw theory was employed to analyze the kinematic properties, and numerical simulations were performed in MATLAB and SolidWorks. The deployable space antenna showed transition from stowed to fully deployed state in just 53 seconds with high stability throughout the deployment process. The TSDAM attained a storage ratio of up to 15.3 for height and volume with 0.01048mm of deformation for a 12 units configuration. Mesh convergence analysis proved the consistency of the simulation results for 415314 tetrahedral shaped elements. The virtual experiments in SolidWorks verified the analytical Screw theory based model and ensured that the design was smooth and flexible for deployment in operational conditions. The research establishes a robust design framework for future deployable antennas, offering enhanced performance, simplified structure, and improved reliability
Related Topics
- Type
- article
- Landing Page
- http://arxiv.org/abs/2511.19287
- https://arxiv.org/pdf/2511.19287
- OA Status
- green
- OpenAlex ID
- https://openalex.org/W7106782949
Raw OpenAlex JSON
- OpenAlex ID
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https://openalex.org/W7106782949Canonical identifier for this work in OpenAlex
- Title
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Innovative Modular Design and Kinematic Approach based on Screw Theory for Triple Scissors Links Deployable Space Antenna MechanismWork title
- Type
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articleOpenAlex work type
- Publication year
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2025Year of publication
- Publication date
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2025-11-24Full publication date if available
- Authors
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Aamir, Mamoon, Sattar Mariyam, Junejo Naveed Ur Rehman, Abbasi, Aqsa ZafarList of authors in order
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https://arxiv.org/abs/2511.19287Publisher landing page
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https://arxiv.org/pdf/2511.19287Direct link to full text PDF
- Open access
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YesWhether a free full text is available
- OA status
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greenOpen access status per OpenAlex
- OA URL
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https://arxiv.org/pdf/2511.19287Direct OA link when available
- Concepts
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Modular design, Kinematics, Software deployment, Antenna (radio), MATLAB, Mechanism (biology), Computer science, Engineering, Solar sail, Reliability (semiconductor), Screw theory, Aperture (computer memory), Stability (learning theory), Reconfigurability, Mechanical engineering, Compliant mechanism, Topology (electrical circuits), Simulation, Structural engineering, Space (punctuation), Configuration design, Aerospace engineering, Deformation (meteorology)Top concepts (fields/topics) attached by OpenAlex
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0Total citation count in OpenAlex
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| abstract_inverted_index.mechanism | 16, 39, 95 |
| abstract_inverted_index.numerical | 138 |
| abstract_inverted_index.performed | 141 |
| abstract_inverted_index.precision | 28 |
| abstract_inverted_index.stability | 124, 164 |
| abstract_inverted_index.SolidWorks | 90, 211 |
| abstract_inverted_index.analytical | 214 |
| abstract_inverted_index.confirming | 113 |
| abstract_inverted_index.deployable | 14, 94, 147, 242 |
| abstract_inverted_index.deployment | 54, 126, 167, 229 |
| abstract_inverted_index.integrity. | 59 |
| abstract_inverted_index.simplified | 247 |
| abstract_inverted_index.simulation | 200 |
| abstract_inverted_index.structural | 58, 123 |
| abstract_inverted_index.structure, | 248 |
| abstract_inverted_index.systematic | 63 |
| abstract_inverted_index.throughout | 165 |
| abstract_inverted_index.transition | 151 |
| abstract_inverted_index.SolidWorks. | 145 |
| abstract_inverted_index.conditions. | 232 |
| abstract_inverted_index.consistency | 197 |
| abstract_inverted_index.convergence | 193 |
| abstract_inverted_index.deformation | 111, 186 |
| abstract_inverted_index.efficiency. | 127 |
| abstract_inverted_index.establishes | 235 |
| abstract_inverted_index.experiments | 209 |
| abstract_inverted_index.operational | 231 |
| abstract_inverted_index.properties, | 136 |
| abstract_inverted_index.reliability | 251 |
| abstract_inverted_index.simulations | 139 |
| abstract_inverted_index.tetrahedral | 204 |
| abstract_inverted_index.(0.01437mm), | 112 |
| abstract_inverted_index.compactness, | 107 |
| abstract_inverted_index.constituting | 81 |
| abstract_inverted_index.deformation. | 98 |
| abstract_inverted_index.observation. | 37 |
| abstract_inverted_index.performance, | 246 |
| abstract_inverted_index.communication | 34 |
| abstract_inverted_index.configuration | 103, 117 |
| abstract_inverted_index.configuration. | 191 |
| abstract_inverted_index.configurations | 80 |
| cited_by_percentile_year | |
| countries_distinct_count | 0 |
| institutions_distinct_count | 4 |
| citation_normalized_percentile.value | 0.73981999 |
| citation_normalized_percentile.is_in_top_1_percent | False |
| citation_normalized_percentile.is_in_top_10_percent | False |