Title :
Modeling and analysis of tether-based mobile robot based on flight experiments
Author :
Hirano, Daichi ; Kobayashi, Akihiro ; Nagaoka, Keizo ; Yoshida, Kenta ; Kato, Haruhisa ; Watanabe, K. ; Ueta, Atsushi ; Abiko, Satoko ; Nishida, Shuichi ; Oda, Masaomi ; Nakanishi, Hayao ; Yoshii, Masahiro ; Suzuki, Satoshi
Author_Institution :
Dept. of Aerosp. Eng., Tohoku Univ., Sendai, Japan
Abstract :
This paper discusses the dynamics of a tether-based mobile robot in space. The tether-based mobile robot is constrained geometrically using several tethers and can move within an area bounded by the tethers´ anchors by changing the tethers´ lengths. This robot is equipped with an extendable and retractable arm that approaches the tethers´ anchor and reposition it to another point for changing the accessible area and covering a wider area. The Japan Aerospace Exploration Agency conducted an experiment called Robot Experiment on Japanese Experimental Module (REX-J) on the International Space Station for demonstrating such a system´s fundamental capabilities. In this paper, the flexibilities of the extendable arm and tethers used in the REX-J are evaluated through image analysis of flight data. This analysis provides the robot´s dynamics in three dimensions, which can not be verified experimentally on the ground. In addition, we propose dynamic models for the extendable arm and the tethers. The proposed models are validated by comparing the flight data and the simulation results obtained using the proposed model.
Keywords :
aerospace robotics; computational geometry; manipulator dynamics; mobile robots; International Space Station; Japan Aerospace Exploration Agency; REX-J; extendable arm; flight data image analysis; flight experiments; retractable arm; robot dynamics; robot experiment-on-Japanese experimental module; tether-based mobile robot analysis; tether-based mobile robot modeling; Robots;
Conference_Titel :
Aerospace Conference, 2014 IEEE
Conference_Location :
Big Sky, MT
Print_ISBN :
978-1-4799-5582-4
DOI :
10.1109/AERO.2014.6836266