Abstract
This study proposes a mechanism for solid surface deployable antennas based on flasher rigid origami. The mechanism scheme design and degree-of-freedom analysis were conducted utilizing a Kirigami release constraint strategy. Subsequently, a spatial geometric model of the key points was established incorporating the folding and unfolding characteristics and geometric relationships within the mechanism. Furthermore, a comprehensive 3D model of the antenna was developed by determining the hinge locations, geometric parameters, and driving mechanism, followed by a kinematic simulation analysis. Finally, a prototype was constructed, and a microgravity deployment experiment was conducted to verify the feasibility of the mechanism.
| Original language | English |
|---|---|
| Article number | 112033 |
| Journal | Thin-Walled Structures |
| Volume | 201 |
| DOIs | |
| State | Published - 1 Aug 2024 |
Keywords
- Flasher origami
- Kinematic analysis
- Mechanism design
- Microgravity environment
- Solid surface deployable antennas
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