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May 28, 2026Aircraft Engineering and Aerospace Technology

Dynamic consistent hierarchical decoupling optimization of modular microsatellite structures for on-orbit assembly

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Authors

YFYanbo FengJYJichang YueZHZhenyang Huang

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Overview

Randomized trial investigates lightweight design optimization for modular satellites, suggesting enhanced assembly efficiency.

Key Points

  • This research aims to develop a dynamic-consistent hierarchical framework for lightweight modular satellite design, focusing on stability under frequency constraints.
  • Reformulated multi-subsystem structures into sequential mass minimization problems.
  • Used a genetic algorithm for optimization within each subsystem.
  • Verified system-level consistency through finite element analysis.
  • Achieved significant lightweight performance while maintaining dynamic stability within the base frequency range.
  • Optimal matching of structural geometric parameters was accomplished using the genetic optimization algorithm.
  • Provided an effective engineering method for modular satellite assembly by space robots or astronauts.

Cite This Study

Feng et al. (2026) studied this question.

synapsesocial.com/papers/6a17dcf93fad632b0f9d9a83https://doi.org/10.1108/aeat-07-2025-0242
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