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 inEuropean journal of control Vol. 70; p. 100782
Main Authors Barman, Saumitra, Sinha, Manoranjan
Format Journal Article
LanguageEnglish
Published Elsevier Ltd 01.03.2023
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