Singularity avoidance controller design for spacecraft attitude control using double-gimbal variable-speed control moment gyro

A sub-optimal singularity avoidance large angle rest-to-rest attitude maneuver control of a rigid spacecraft actuated using a double-gimbal variable-speed control moment gyro (DGVSCMG) is proposed for avoiding the control torque saturation and the gimbal lock singularity. To achieve this objective,...

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Bibliographic Details

Published in:	European journal of control Vol. 70; p. 100782
Main Authors:	Barman, Saumitra, Sinha, Manoranjan
Format:	Journal Article
Language:	English
Published:	Elsevier Ltd 01.03.2023
Subjects:	Attitude control DGVSCMG Gimbal-lock Model predictive static programming Singularities Attitude control Singularities Model predictive static programming Gimbal-lock DGVSCMG
ISSN:	0947-3580, 1435-5671
Online Access:	Get full text
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