Abstract
A ultra-large spacecraft is a significant space infrastructure for the exploration and utilization of space resources, and also an important aerospace equipment to achieve the goal of becoming a powerful space nation.With its ultra-large size, ultra-flexible structure, and ultra-low fundamental frequency, ultra-large spacecrafts present new challenges in terms of dynamic modeling, numerical analysis, precise attitude control, low-frequency vibration suppression, and wave characteristics adjustment.This paper introduces our research progress for the above problems based on symplectic methods, including on-orbit coupling dynamics and attitude control, wave analysis and control, design of deployable space structures, and variable-stiffness active control methods.
| Translated title of the contribution | Reviews on symplectic method for dynamics and control of ultra-large space structures |
|---|---|
| Original language | Chinese (Traditional) |
| Pages (from-to) | 108-117 |
| Number of pages | 10 |
| Journal | Jisuan Lixue Xuebao/Chinese Journal of Computational Mechanics |
| Volume | 41 |
| Issue number | 1 |
| DOIs | |
| State | Published - Feb 2024 |
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