Development of a Multi-Axial Force Sensor for Small Satellite Docking-Reference-Cited by-同舟云学术

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Development of a Multi-Axial Force Sensor for Small Satellite Docking

Published:2024-06-03 Issue: Volume:22 Page:152-156
ISSN:
Container-title:2024 11th International Workshop on Metrology for AeroSpace (MetroAeroSpace)
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Author:

Veronese Matteo¹,Caon Alex¹,Giubilato Riccardo²,Branz Francesco³,Francesconi Alessandro³

Affiliation:

1. University of Padova,Centre of Studies and Activities for Space “G. Colombo”,Padova,Italy

2. Institute of Robotics and Mechatronics,German Aerospace Center (DLR),Wessling,Germany

3. University of Padova,Department of Industrial Engineering,Padova,Italy

Publisher

IEEE

Link

http://xplorestaging.ieee.org/ielx8/10591476/10591509/10591564.pdf?arnumber=10591564

Reference7 articles.

1. Ultra-soft electromagnetic docking with applications to in-orbit assembly;Foust;69th International Astronautical Congress, Bremen, Germany,2018

2. Design, manufacture, test and experiment of six-axis force torque sensor for chinese experimental module manipulator;Sun;Sensors,2022

3. Impedance-based contact control of a free-flying space robot with respect to coefficient of restitution

4. Miniature docking mechanism for cubesats;Branz;Acta Astronautica,2020

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