DocumentCode
592779
Title
Development of an eddy current brake system for detumbling malfunctioning satellites
Author
Sugai, Fumihito ; Abiko, Satoko ; Tsujita, Teppei ; Xin Jiang ; Uchiyama, Masaru
Author_Institution
Dept. of Mech. Syst. & Design, Tohoku Univ., Sendai, Japan
fYear
2012
fDate
16-18 Dec. 2012
Firstpage
325
Lastpage
330
Abstract
This paper proposes a new method to detumble uncontrolled large space debris such as malfunctioning satellites. There are many researches about a space robot capturing and deorbiting space debris. However it is generally very difficult to capture tumbling targets such as the malfunctioning satellites because these targets are out of control in attitude and rotate with nutational motion. Hence we propose a new way to detumble them with an eddy current brake. The eddy current brake can detumble the uncontrolled targets without any contact. In this paper, we describe design and development of a linear induction motor type of eddy current brake. Experimental verification is carried out to verify the performance of the developed eddy current brake in order to fulfill the requirement for detumbling the uncontrolled satellite.
Keywords
aerospace robotics; artificial satellites; attitude control; eddy current braking; linear induction motors; space debris; attitude control; deorbiting; eddy current brake system development; linear induction motor; malfunctioning satellite detumbling method; performance verification; rotation control; space robot; uncontrolled large space debris; uncontrolled satellite detumbling; Coils; Eddy currents; Force; Robots; Satellites; Space vehicles; Vectors;
fLanguage
English
Publisher
ieee
Conference_Titel
System Integration (SII), 2012 IEEE/SICE International Symposium on
Conference_Location
Fukuoka
Print_ISBN
978-1-4673-1496-1
Type
conf
DOI
10.1109/SII.2012.6427330
Filename
6427330
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