摘要
Locomotion in confined microgravity environments, such as spacecraft piping, presents unique challenges due to the lack of gravitational normal forces and the strict requirement for environmental safety. Traditional rigid-body controllers often struggle to generate sufficient traction for agile maneuvering without violating the structural limits of fragile surroundings. This article introduces a novel control framework for a 6-link spinal wheeled-legged robot that actively exploits internal spinal dynamics to steer the system. We propose a lie-algebraic error-state model predictive control that plans optimal momentum fluxes and spinal configurations, ensuring singularity-free tracking even during omnidirectional tumbling. To guarantee safety, a hierarchical whole-body controller enforces strict environment-admissible force constraints and integrates an event-triggered asymmetric friction adaptation strategy to handle uncertain surface properties. Uniquely, the proposed framework is validated through real-world on-orbit experiments using a flight-equivalent pipe testbed aboard the China Space Station. Results demonstrate that our method successfully achieves agile heading recovery where rigid-body baselines fail to converge due to traction loss, while strictly maintaining contact forces within the 6.6 N safety limit despite friction uncertainties.
| 源语言 | 英语 |
|---|---|
| 期刊 | IEEE Transactions on Industrial Electronics |
| DOI | |
| 出版状态 | 已接受/待刊 - 2026 |
| 已对外发布 | 是 |
指纹
探究 'Active Momentum Control for Spinal In-Pipe Robots in Microgravity: On-Orbit Validation' 的科研主题。它们共同构成独一无二的指纹。引用此
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