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Capture and removal of large space debris is needed to prevent the growth of the debris population in low Earth orbit. Capture of a non-cooperative object by a manipulator mounted on a chaser satellite requires collision-free trajectory of the manipulator. The obstacle vector field (OVF) method allows to solve the trajectory planning problem in difficult scenarios. The OVF method is based on a vector field that surrounds the obstacles and generates virtual forces that drive the manipulator around the obstacles. The original formulation of the OVF method allows to obtain the desired position of the gripper, but not the desired orientation. To perform the grasping manoeuvre, the gripper has to be positioned in a specific point and aligned with the grasping interface. In this paper, we propose a modification to the OVF method that allows to obtain the desired position and orientation of the gripper. Moreover, we investigate the practical applicability of the OVF method. The OVF method is demonstrated in experiments performed on a planar air-bearing microgravity simulator. The presented results prove that the OVF method can be applied for a real system operating in simulated microgravity conditions.
Rocznik
Strony
171--187
Opis fizyczny
Bibliogr. 39 poz., rys., tab.
Twórcy
autor
- Centrum Badań Kosmicznych Polskiej Akademii Nauk (CBK PAN), Warsaw, Poland
autor
- Centrum Badań Kosmicznych Polskiej Akademii Nauk (CBK PAN), Warsaw, Poland
autor
- Centrum Badań Kosmicznych Polskiej Akademii Nauk (CBK PAN), Warsaw, Poland
autor
- Centrum Badań Kosmicznych Polskiej Akademii Nauk (CBK PAN), Warsaw, Poland
Bibliografia
- Basmadji F.L., Chmaj G., Rybus T., Seweryn K. (2019) Microgravity testbed for the development of space robot control systems and the demonstration of orbital maneuvers, Proceedings of SPIE: Photonics Applications in Astronomy, Communications, Industry, and High-Energy Physics Experiments, 111763V, Wilga, Poland.
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- Rybus T., Seweryn K. (2016) Planar air-bearing microgravity simulators: review of applications, existing solutions and design parameters, Acta Astronautica, Vol. 120, 239-259.
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Typ dokumentu
Bibliografia
Identyfikator YADDA
bwmeta1.element.baztech-36544e25-07e2-4b3c-a6fa-157b654c0eef