Surrogate Modeling Accelerated Shape Optimization of Deployable Composite Tape-Spring Hinges
Author:
Affiliation:
1. Xi’an Jiaotong University, 710049 Xi’an, People’s Republic of China
2. Sichuan University, 610065 Chengdu, People’s Republic of China
3. Xi’an Institute of Space Radio Technology, 710100 Xi’an, People’s Republic of China
Funder
Shanghai Rising-Star Program
National Natural Science Foundation of China
Fundamental Research Funds for the Central Universities
Open Project of State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiaotong University
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061668
Reference37 articles.
1. Deployment Analysis of the Lenticular Jointed Antennas Onboard the Mars Express Spacecraft
2. Lenticular Jointed Antenna Deployment Anomaly and Resolution Onboard the Mars Express Spacecraft
3. Composite Tube Hinges
4. Multivariate Rational Response Surface Approximation of Nodal Displacements of Truss Structures
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