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Robust CMG steering logic with gimbal angle constraints

Lappas, V and Wie, B (2006) Robust CMG steering logic with gimbal angle constraints

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Advances in microelectronics and small satellite engineering have enabled the development of micro Control Moment Gyros (CMG) for agile spacecraft control. CMGs come with a condition referred to as singularity where for a particular gimbal angle geometric configuration they cannot produce control torque along a certain direction. The paper describes a robust CMG steering logic for CMGs with a mechanical gimbal angle constraint. Copyright © 2006 by the American Institute of Aeronautics and Astronautics, Inc, All rights reserved.

Item Type: Conference or Workshop Item (UNSPECIFIED)
Divisions : Surrey research (other units)
Authors :
Wie, B
Date : 1 December 2006
Depositing User : Symplectic Elements
Date Deposited : 17 May 2017 11:25
Last Modified : 23 Jan 2020 16:50

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