DocumentCode :
2595743
Title :
Launching penetrator by casting manipulator system
Author :
Arisumi, Hitoshi ; Otsuki, Masatsugu ; Nishida, Shinichiro
Author_Institution :
Intell. Syst. Res. Inst., Nat. Inst. of Adv. Ind. Sci. & Technol. (AIST), Tsukuba, Japan
fYear :
2012
fDate :
7-12 Oct. 2012
Firstpage :
5052
Lastpage :
5058
Abstract :
Supposing a space mission of setting monitoring devices at suitable positions on the moon, we discuss how to apply a casting manipulation to the mission. This paper addresses a mechanism of a casting manipulator system and control method to launch a penetrator to the desired position. First, we discuss launching methods, and focus on a method by using rotation of a boom. We then propose the mechanism that keeps a posture of the penetrator equipped at the tip of the boom constant for the absolute coordinate system during its rotation. This mechanism prevents the wire which connects the penetrator and the robot´s base from winding the boom. Analyzing a position error of landing point caused by delay of releasing the penetrator, we propose the motion control of the boom to reduce the error. Finally, we develop the system and verify the effectiveness of the proposed method through experiment.
Keywords :
aerospace robotics; delays; motion control; path planning; planetary rovers; wires; absolute coordinate system; casting manipulator control method; casting manipulator system; delay; landing point; monitoring device setting; moon positions; motion control; penetrator launching methods; position error; space mission; Casting; Manipulators; Moon; Timing; Trajectory; Wires; launching; manipulation; penetrator; space robotics;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Robots and Systems (IROS), 2012 IEEE/RSJ International Conference on
Conference_Location :
Vilamoura
ISSN :
2153-0858
Print_ISBN :
978-1-4673-1737-5
Type :
conf
DOI :
10.1109/IROS.2012.6386078
Filename :
6386078
Link To Document :
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