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
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