Dezhi Zhang;Guocai Yang;Junhong Ji;Shaowei Fan;Minghe Jin;Hong Liu
{"title":"Constrained Visual Servoing for Capturing Adapter Rings on Tumbling Satellites With a Free-Floating Robot","authors":"Dezhi Zhang;Guocai Yang;Junhong Ji;Shaowei Fan;Minghe Jin;Hong Liu","doi":"10.1109/TAES.2024.3523461","DOIUrl":null,"url":null,"abstract":"This article proposes a constrained visual servoing method for the safe and reliable capture of noncooperative tumbling satellites using a free-floating space robot. The adapter ring serves as both the capture interface and the visual feature. However, during the close-range fine servoing phase, only a limited portion of the adapter ring is visible within the hand–eye camera's field of view due to its large size, leading to reduced servoing accuracy. To address this issue, a three-line structured light system is introduced in this phase to augment visual features and complement the long-range guidance provided by the monocular camera. This scheme enables visual servoing from long to close range. Moreover, the target's tumbling motion, the ring's geometric properties, and the coupled dynamics between the manipulator and the base pose significant challenges to the reliability and safety of the servoing process. To mitigate these issues, a set of constraints is formulated, including hard constraints to ensure that visual features remain within the camera's field of view and to avoid obstacles, as well as soft constraints to maintain continuous communication with the ground station and minimize impact forces at the moment of capture. To manage these constraints and regulate the system in real time, a motion planner employing nonlinear model-predictive control is developed, supported by differential models of visual features. Furthermore, a low-level joint controller based on quadratic programming ensures accurate tracking of planned trajectories while adhering to torque limits. Simulation results validate the effectiveness of the proposed method.","PeriodicalId":13157,"journal":{"name":"IEEE Transactions on Aerospace and Electronic Systems","volume":"61 3","pages":"6026-6040"},"PeriodicalIF":5.7000,"publicationDate":"2024-12-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"IEEE Transactions on Aerospace and Electronic Systems","FirstCategoryId":"94","ListUrlMain":"https://ieeexplore.ieee.org/document/10816611/","RegionNum":2,"RegionCategory":"计算机科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0
Abstract
This article proposes a constrained visual servoing method for the safe and reliable capture of noncooperative tumbling satellites using a free-floating space robot. The adapter ring serves as both the capture interface and the visual feature. However, during the close-range fine servoing phase, only a limited portion of the adapter ring is visible within the hand–eye camera's field of view due to its large size, leading to reduced servoing accuracy. To address this issue, a three-line structured light system is introduced in this phase to augment visual features and complement the long-range guidance provided by the monocular camera. This scheme enables visual servoing from long to close range. Moreover, the target's tumbling motion, the ring's geometric properties, and the coupled dynamics between the manipulator and the base pose significant challenges to the reliability and safety of the servoing process. To mitigate these issues, a set of constraints is formulated, including hard constraints to ensure that visual features remain within the camera's field of view and to avoid obstacles, as well as soft constraints to maintain continuous communication with the ground station and minimize impact forces at the moment of capture. To manage these constraints and regulate the system in real time, a motion planner employing nonlinear model-predictive control is developed, supported by differential models of visual features. Furthermore, a low-level joint controller based on quadratic programming ensures accurate tracking of planned trajectories while adhering to torque limits. Simulation results validate the effectiveness of the proposed method.
期刊介绍:
IEEE Transactions on Aerospace and Electronic Systems focuses on the organization, design, development, integration, and operation of complex systems for space, air, ocean, or ground environment. These systems include, but are not limited to, navigation, avionics, spacecraft, aerospace power, radar, sonar, telemetry, defense, transportation, automated testing, and command and control.