Design and dynamics of space- station-based one-degree-of-freedom repeatedly deployable exposure platform

For cosmic-dust experiments on the space station, this paper proposes a one-degree-of-freedom repeatedly deployable exposure platform supporting multiple panels. A 4-panel module forms the basic unit and, through a modular library, scales to any panel count with a folding ratio of 14.09 : (1) a uniform acceleration-deceleration driving strategy at the control end or motor is proposed. Kinematic models define the motion space for arbitrary panel numbers. Lagrange dynamics models predict torque demand versus panel number and deployment period. For the 4-panel case, the two strategies need 0.0777 N m and 0.0972 N m at 40 s; with a 1 N m target the minimum periods shorten to 14.05 s and 12.63 s. A 4-panel prototype verified smooth, synchronized deploy-retract. Positioning tests showed absolute accuracies better than 5.42 ± 0.60 mm and repeatability finer than 46 ± 2 μm on all axes, providing a validated basis for future space exposure platforms.

Authors

Institutions

Publication Details

Journal
iScience
Published
2025-08-18
DOI
https://doi.org/10.1016/j.isci.2025.113390
Primary Topic
Space Satellite Systems and Control
Type
article
Field-Weighted Citation Impact
0.00
Controls
|||
ALL TIME
JAN
FEB
MAR
APR
MAY
JUN
JUL
AUG
SEP
OCT
article

Design and dynamics of space- station-based one-degree-of-freedom repeatedly deployable exposure platform

Xihan Li, Bong-Seok Kang, Haifeng Zhao, Chong Zhao et al.
iScience
Space Satellite Systems and Control
article

Design and dynamics of space- station-based one-degree-of-freedom repeatedly deployable exposure platform

Xihan Li, Bong-Seok Kang, Haifeng Zhao, Chong Zhao, Ke Wang, Yutong Wang, Letian Wang, Dong Guo, Junjie Li
article en

Abstract

For cosmic-dust experiments on the space station, this paper proposes a one-degree-of-freedom repeatedly deployable exposure platform supporting multiple panels. A 4-panel module forms the basic unit and, through a modular library, scales to any panel count with a folding ratio of 14.09 : (1) a uniform acceleration-deceleration driving strategy at the control end or motor is proposed. Kinematic models define the motion space for arbitrary panel numbers. Lagrange dynamics models predict torque demand versus panel number and deployment period. For the 4-panel case, the two strategies need 0.0777 N m and 0.0972 N m at 40 s; with a 1 N m target the minimum periods shorten to 14.05 s and 12.63 s. A 4-panel prototype verified smooth, synchronized deploy-retract. Positioning tests showed absolute accuracies better than 5.42 ± 0.60 mm and repeatability finer than 46 ± 2 μm on all axes, providing a validated basis for future space exposure platforms.

iScienceVol. 28(9)
Chinese Academy of Sciences (CN), Technology and Engineering Center for Space Utilization (CN), University of Chinese Academy of Sciences (CN)
Peace, Justice and strong institutions
Openalex Percentile: Top 71%
Space Satellite Systems and Control
AI Navigator

Ask Laika to Summarize, Analyze, and Connect papers live on the map.

Summarize Papers & Methodologies

Extract key findings, datasets, and comparative methods across publications.

Benchmark Rankings & Visual Analytics

Rank top research institutions, authors, funders, topics, and journals by Field-Weighted Citation Impact (FWCI) and paper volume with instant charts.

Connect Distant Disciplines

Bridge topological clusters on the map to find hidden collaborative intersections.

Design and dynamics of space- station-based one-degree-of-freedom repeatedly deployable exposure platform — Xihan Li, Bong-Seok Kang, et al. · iScience (2025) | TGRS Research Map | TGRS