Morphology and Behavior Co-Optimization of Modular Satellites for Attitude Control
Yuxing Wang, Jie Li, Cong Yu, Xinyang Li, Simeng Huang, Yongzhe Chang,, Xueqian Wang, Bin Liang

TL;DR
This paper presents a gradient-based co-optimization method for modular satellites, improving attitude control performance by simultaneously optimizing morphology and control strategies, outperforming traditional evolution-based methods.
Contribution
Introduces a novel gradient-based co-optimization approach for modular satellite design and control, addressing the complex bi-level optimization challenge.
Findings
Better mission performance compared to evolution-based designs
More efficient and practical assembly strategies
Enhanced flexibility and resilience in satellite architecture
Abstract
The emergence of modular satellites marks a significant transformation in spacecraft engineering, introducing a new paradigm of flexibility, resilience, and scalability in space exploration endeavors. In addressing complex challenges such as attitude control, both the satellite's morphological architecture and the controller are crucial for optimizing performance. Despite substantial research on optimal control, there remains a significant gap in developing optimized and practical assembly strategies for modular satellites tailored to specific mission constraints. This research gap primarily arises from the inherently complex nature of co-optimizing design and control, a process known for its notorious bi-level optimization loop. Conventionally tackled through artificial evolution, this issue involves optimizing the morphology based on the fitness of individual controllers, which is…
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Taxonomy
TopicsSpace Satellite Systems and Control · Spacecraft Design and Technology · Spacecraft Dynamics and Control
