Abstract
Recently, large space structures are being developed. From the point of view of payload capacity and transportation efficiency, large space structures are required to be lightweight and highly efficient in their folding. Cable-panel structures are also expected to satisfy the above conditions mainly due to the omission of frames that hold panels structures. However, the deployment of three-dimensional membranes is difficult to control accurately because of the small stiffness normal to membranes. In this study, we discuss the wire location design in the wire-based deployment of three-dimensional plates. And, through experiments, we evaluate 27 design locations of wires for deployment and compare the deployed shape between the designed dimensions and the measured surface. Then, we confirmed the increment of 2.2 percent in height dimension. Furthermore, we confirmed that our proposed deployment method is feasible, and obtained several design criteria for wire design: First, it is necessary to consider an order of deployment to deploy from the outside surface. Second, the design needs to intersect folds at right angles. Third, extending the length of designs without changing the route shape of the designs leads to higher accuracy of the deployment shape without causing a large increase in the required forces. The multi particle system model was applied to predict the deformation of the structure reasonablly.
| Original language | English |
|---|---|
| Title of host publication | 4th AIAA Spacecraft Structures Conference, 2017 |
| Publisher | American Institute of Aeronautics and Astronautics Inc, AIAA |
| ISBN (Print) | 9781624104558 |
| Publication status | Published - 2017 |
| Event | 4th AIAA Spacecraft Structures Conference, 2017 - Grapevine, United States Duration: 2017 Jan 9 → 2017 Jan 13 |
Other
| Other | 4th AIAA Spacecraft Structures Conference, 2017 |
|---|---|
| Country | United States |
| City | Grapevine |
| Period | 17/1/9 → 17/1/13 |
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ASJC Scopus subject areas
- Electrical and Electronic Engineering
- Aerospace Engineering
- Mechanical Engineering
- Computer Science Applications
Cite this
A study on the design of deployable cable-panel structure. / Seino, Koujirou; Parque Tenorio, Victor; Miyashita, Tomoyuki.
4th AIAA Spacecraft Structures Conference, 2017. American Institute of Aeronautics and Astronautics Inc, AIAA, 2017.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - A study on the design of deployable cable-panel structure
AU - Seino, Koujirou
AU - Parque Tenorio, Victor
AU - Miyashita, Tomoyuki
PY - 2017
Y1 - 2017
N2 - Recently, large space structures are being developed. From the point of view of payload capacity and transportation efficiency, large space structures are required to be lightweight and highly efficient in their folding. Cable-panel structures are also expected to satisfy the above conditions mainly due to the omission of frames that hold panels structures. However, the deployment of three-dimensional membranes is difficult to control accurately because of the small stiffness normal to membranes. In this study, we discuss the wire location design in the wire-based deployment of three-dimensional plates. And, through experiments, we evaluate 27 design locations of wires for deployment and compare the deployed shape between the designed dimensions and the measured surface. Then, we confirmed the increment of 2.2 percent in height dimension. Furthermore, we confirmed that our proposed deployment method is feasible, and obtained several design criteria for wire design: First, it is necessary to consider an order of deployment to deploy from the outside surface. Second, the design needs to intersect folds at right angles. Third, extending the length of designs without changing the route shape of the designs leads to higher accuracy of the deployment shape without causing a large increase in the required forces. The multi particle system model was applied to predict the deformation of the structure reasonablly.
AB - Recently, large space structures are being developed. From the point of view of payload capacity and transportation efficiency, large space structures are required to be lightweight and highly efficient in their folding. Cable-panel structures are also expected to satisfy the above conditions mainly due to the omission of frames that hold panels structures. However, the deployment of three-dimensional membranes is difficult to control accurately because of the small stiffness normal to membranes. In this study, we discuss the wire location design in the wire-based deployment of three-dimensional plates. And, through experiments, we evaluate 27 design locations of wires for deployment and compare the deployed shape between the designed dimensions and the measured surface. Then, we confirmed the increment of 2.2 percent in height dimension. Furthermore, we confirmed that our proposed deployment method is feasible, and obtained several design criteria for wire design: First, it is necessary to consider an order of deployment to deploy from the outside surface. Second, the design needs to intersect folds at right angles. Third, extending the length of designs without changing the route shape of the designs leads to higher accuracy of the deployment shape without causing a large increase in the required forces. The multi particle system model was applied to predict the deformation of the structure reasonablly.
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M3 - Conference contribution
AN - SCOPUS:85017372101
SN - 9781624104558
BT - 4th AIAA Spacecraft Structures Conference, 2017
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
ER -