Abstract
This paper presents an analysis of the capture of an uncontrolled target satellite by a manipulator mounted on a chaser spacecraft. We compare our novel technique, called tangent capture, with two other well-known approaches: free-floating and forced synchronous motion. In the proposed approach, the chaser has only initial linear velocity. The analysis takes the form of a numerical simulation performed on a three-dimensional system. Performance is evaluated using three parameters: (i) control torques in the manipulator’s joints; (ii) time to eventual collision between system components; and (iii) reaction torque and force in the gripper. The evaluation demonstrates that the tangent capture scenario improves the values of all analyzed parameters.
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The project, titled “Mobility of a nonholonomic space robot constrained by large movable obstacles” was financed by the Polish National Science Center under research grant 2015/17/B/ST7/03995.
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Acknowledgements
Karol Seweryn thanks Prof. Krzysztof Tchoń from Wroclaw University of Technology for their fruitful discussions about space robots and nonholonomic systems.
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This research was funded by CBK PAN.
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Seweryn, K., Basmadji, F.L. & Rybus, T. Space Robot Performance During Tangent Capture of an Uncontrolled Target Satellite. J Astronaut Sci 69, 1017–1047 (2022). https://doi.org/10.1007/s40295-022-00330-2
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DOI: https://doi.org/10.1007/s40295-022-00330-2