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,...
Saved in:
Published in | European journal of control Vol. 70; p. 100782 |
---|---|
Main Authors | , |
Format | Journal Article |
Language | English |
Published |
Elsevier Ltd
01.03.2023
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
Be the first to leave a comment!