Shorter Path Design and Control for an Underactuated Satellite

In the event of a control failure on an axis of a spacecraft, a target attitude can be achieved by several sequential rotations around the remaining control axes. For a spacecraft actuating with wheels, the form of each submaneuver should be a pure single axis rotation since the failed axis should n...

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Bibliographic Details

Published in:	International journal of aerospace engineering Vol. 2017; no. 2017; pp. 1 - 9
Main Authors:	Oh, Hwa-Suk, Kim, Jichul, Kim, Donghoon, Lee, Jung-Hyung
Format:	Journal Article
Language:	English
Published:	Cairo, Egypt Hindawi Publishing Corporation 01-01-2017 Hindawi Hindawi Limited
Subjects:	Aerospace engineering
Online Access:	Get full text
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