Paper Abstract and Keywords |
Presentation |
2006-07-13 15:40
Failure Analysis and Simulation of Electrical Power System for Satellite Go Segami, Hiroaki Kusawake, Yasuhiro Shimizu, Koichi Kibe (JAXA) EE2006-15 |
Abstract |
(in Japanese) |
(See Japanese page) |
(in English) |
Fault tolerant desigen is necessary for satellite because we can’t repair anything in space if there is something wrong with the satellite. Even if the satellite has the trouble, we have to minimize damage and carry out missions. Therefore we perform enough tests and simulations on the ground and improve reliability by reflecting the results of the design. In this paper, we discuss failure analysis of short circuit and disconnection fault which are the failure modes of the electrical power system for the satellite. |
Keyword |
(in Japanese) |
(See Japanese page) |
(in English) |
Power System for Satellite / Open Failure / Harness / Fuse / Transient Response / / / |
Reference Info. |
IEICE Tech. Rep., vol. 106, no. 152, EE2006-15, pp. 35-39, July 2006. |
Paper # |
EE2006-15 |
Date of Issue |
2006-07-06 (EE) |
ISSN |
Print edition: ISSN 0913-5685 Online edition: ISSN 2432-6380 |
Copyright and reproduction |
All rights are reserved and no part of this publication may be reproduced or transmitted in any form or by any means, electronic or mechanical, including photocopy, recording, or any information storage and retrieval system, without permission in writing from the publisher. Notwithstanding, instructors are permitted to photocopy isolated articles for noncommercial classroom use without fee. (License No.: 10GA0019/12GB0052/13GB0056/17GB0034/18GB0034) |
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EE2006-15 |
Conference Information |
Committee |
EE |
Conference Date |
2006-07-13 - 2006-07-14 |
Place (in Japanese) |
(See Japanese page) |
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Paper Information |
Registration To |
EE |
Conference Code |
2006-07-EE |
Language |
Japanese |
Title (in Japanese) |
(See Japanese page) |
Sub Title (in Japanese) |
(See Japanese page) |
Title (in English) |
Failure Analysis and Simulation of Electrical Power System for Satellite |
Sub Title (in English) |
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Keyword(1) |
Power System for Satellite |
Keyword(2) |
Open Failure |
Keyword(3) |
Harness |
Keyword(4) |
Fuse |
Keyword(5) |
Transient Response |
Keyword(6) |
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Keyword(7) |
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Keyword(8) |
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1st Author's Name |
Go Segami |
1st Author's Affiliation |
Japan AerospaceExploration Agency (JAXA) |
2nd Author's Name |
Hiroaki Kusawake |
2nd Author's Affiliation |
Japan AerospaceExploration Agency (JAXA) |
3rd Author's Name |
Yasuhiro Shimizu |
3rd Author's Affiliation |
Japan AerospaceExploration Agency (JAXA) |
4th Author's Name |
Koichi Kibe |
4th Author's Affiliation |
Japan AerospaceExploration Agency (JAXA) |
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Speaker |
Author-1 |
Date Time |
2006-07-13 15:40:00 |
Presentation Time |
30 minutes |
Registration for |
EE |
Paper # |
EE2006-15 |
Volume (vol) |
vol.106 |
Number (no) |
no.152 |
Page |
pp.35-39 |
#Pages |
5 |
Date of Issue |
2006-07-06 (EE) |
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