TY - JOUR
T1 - Surrogate-assisted evolutionary optimization and microgravity experimental validation of a planar deployable mechanism
AU - Liu, Bohan
AU - Tan, Jingcheng
AU - Lyu, Haowen
AU - Zhang, Zhengyi
AU - Liu, Zhengyu
AU - Huang, Hai
N1 - Publisher Copyright:
© 2025 Elsevier Masson SAS.
PY - 2026/1
Y1 - 2026/1
N2 - This paper proposes a surrogate-assisted evolutionary framework to optimize the design parameters of a novel planar deployable mechanism, with experimental validation conducted through microgravity tests. The mechanism features an elastic outer frame integrated with an inner rope net, utilizing stored strain energy for passive deployment to overcome the transient operational time limitations of traditional designs. The highly nonlinear deployment dynamics and computationally expensive simulations pose significant challenges for conventional optimization methods. To address this, a Genetic Algorithm (GA) is integrated with Response Surface Methodology (RSM) and Kriging surrogate models to efficiently minimize the maximum backward penetration length during deployment. A parallel evaluation strategy is implemented to significantly reduce the optimization time compared to conventional approaches. Comparative analysis demonstrates the superior performance of the Kriging model, which shows a substantial reduction in maximum residual error compared to the polynomial RSM. Experimental validation under microgravity conditions confirmed the accuracy of the mechanism simulation, and the optimal design successfully deployed with intrusion depths within required limits. The proposed methodology provides an efficient and reliable approach for optimizing complex deployable structures involving computationally expensive simulations.
AB - This paper proposes a surrogate-assisted evolutionary framework to optimize the design parameters of a novel planar deployable mechanism, with experimental validation conducted through microgravity tests. The mechanism features an elastic outer frame integrated with an inner rope net, utilizing stored strain energy for passive deployment to overcome the transient operational time limitations of traditional designs. The highly nonlinear deployment dynamics and computationally expensive simulations pose significant challenges for conventional optimization methods. To address this, a Genetic Algorithm (GA) is integrated with Response Surface Methodology (RSM) and Kriging surrogate models to efficiently minimize the maximum backward penetration length during deployment. A parallel evaluation strategy is implemented to significantly reduce the optimization time compared to conventional approaches. Comparative analysis demonstrates the superior performance of the Kriging model, which shows a substantial reduction in maximum residual error compared to the polynomial RSM. Experimental validation under microgravity conditions confirmed the accuracy of the mechanism simulation, and the optimal design successfully deployed with intrusion depths within required limits. The proposed methodology provides an efficient and reliable approach for optimizing complex deployable structures involving computationally expensive simulations.
KW - Deployment mechanism
KW - Evolutionary algorithm
KW - Mechanism dynamics
KW - Microgravity experiment
KW - Surrogate-assisted optimization
UR - https://www.scopus.com/pages/publications/105023507011
U2 - 10.1016/j.ast.2025.111299
DO - 10.1016/j.ast.2025.111299
M3 - 文章
AN - SCOPUS:105023507011
SN - 1270-9638
VL - 168
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 111299
ER -