In this article, a pyramid-type single-gimbal control moment gyro system mounted on a space structure is employed to realize the integrated control of singularity avoidance attitude maneuver and vibration suppression. The rest-to-rest attitude maneuver is divided into three sections, in which null motion is applied to achieve the above two objects leading to a better control performance. The effectiveness of the proposed control strategy is verified using numerical simulation examples.
Integrated Control of Attitude Maneuver and Vibration Suppression Using Pyramid-Type SGCMGs
IEEE Transactions on Aerospace and Electronic Systems ; 58 , 1 ; 17-26
2022-02-01
4637709 byte
Article (Journal)
Electronic Resource
English
Pointing control of spacecraft using two SGCMGs via LPV control theory
Elsevier | 2010
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