On-orbit servicing is a key enabler of space sustainability, allowing maintenance, refueling, repairs, and upgrades of satellites to extend their operational life. A typical mission involves rendezvous, relative motion synchronization, and final capture with a robotic arm. This work focuses on the capture phase, where safety and reliability requirements meet the challenges of autonomous navigation and control. The target is uncooperative and slowly tumbling, so residual relative motion remains at capture. To address this, a trajectory planning framework is proposed in free-flying mode, where arm and platform are jointly controlled. An enhanced Rapidly-exploring Random Tree (RRT) planner ensures safe maneuvers, and the guidance algorithm is validated on a high-fidelity model including full 3D manipulator dynamics. Experimental tests are performed on a granite-table facility with a frictionless satellite mock-up (representing the target) and a 6-DOF robotic arm moving on a linear rail (representing the chaser). The facility integrates a metrology system to track the platforms’ position and orientation in real time, ensuring precise measurement of grasping performance. The study demonstrates the effectiveness of the proposed GNC architecture in achieving successful manipulation, while also identifying key limitations related to relative kinematic state critical factors, such as relative velocity, orientation misalignment, and contact dynamics.

Experimental Evaluation of Robotic Grasping Strategies for On-Orbit Servicing / Madonna, David Paolo; Carattoli, Matteo; Angeletti, Federica; Pontani, Mauro; Gasbarri, Paolo; Sabatini, Marco. - (2025), pp. 258-271. ( 76th International Astronautical Congress, IAC 2025 Sydney ) [10.52202/083088-0028].

Experimental Evaluation of Robotic Grasping Strategies for On-Orbit Servicing

Madonna, David Paolo;Carattoli, Matteo;Angeletti, Federica;Pontani, Mauro;Gasbarri, Paolo;Sabatini, Marco
2025

Abstract

On-orbit servicing is a key enabler of space sustainability, allowing maintenance, refueling, repairs, and upgrades of satellites to extend their operational life. A typical mission involves rendezvous, relative motion synchronization, and final capture with a robotic arm. This work focuses on the capture phase, where safety and reliability requirements meet the challenges of autonomous navigation and control. The target is uncooperative and slowly tumbling, so residual relative motion remains at capture. To address this, a trajectory planning framework is proposed in free-flying mode, where arm and platform are jointly controlled. An enhanced Rapidly-exploring Random Tree (RRT) planner ensures safe maneuvers, and the guidance algorithm is validated on a high-fidelity model including full 3D manipulator dynamics. Experimental tests are performed on a granite-table facility with a frictionless satellite mock-up (representing the target) and a 6-DOF robotic arm moving on a linear rail (representing the chaser). The facility integrates a metrology system to track the platforms’ position and orientation in real time, ensuring precise measurement of grasping performance. The study demonstrates the effectiveness of the proposed GNC architecture in achieving successful manipulation, while also identifying key limitations related to relative kinematic state critical factors, such as relative velocity, orientation misalignment, and contact dynamics.
2025
76th International Astronautical Congress, IAC 2025
In-orbit servicing; docking; berthing; formation flying; relative dynamics; space robotics
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Experimental Evaluation of Robotic Grasping Strategies for On-Orbit Servicing / Madonna, David Paolo; Carattoli, Matteo; Angeletti, Federica; Pontani, Mauro; Gasbarri, Paolo; Sabatini, Marco. - (2025), pp. 258-271. ( 76th International Astronautical Congress, IAC 2025 Sydney ) [10.52202/083088-0028].
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1765105
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