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Qinglei Hu, Guangfu Ma. Adaptive Variable Structure Maneuvering Control and Vibration Reduction of Three-axis Stabilized Flexible Spacecraft. Eur. J. Control, 12(6):654-668, 2006. [doi]
Possibly Related PublicationsThe following publications are possibly variants of this publication: Reference Model Variable Structure Output Feedback for Attitude Maneuvers Control of Flexible SpacecraftsQinglei Hu, Xiaozhi Gao, Guangfu Ma. iasc, 15(1):53-62, 2009. [doi] FEL-Based Adaptive Dynamic Inverse Control for Flexible Spacecraft Attitude ManeuverYaqiu Liu, Guangfu Ma, Qinglei Hu. isnn 2004: 42-51 [doi] Simultaneous Vibration Reduction and Attitude Control of Flexible Spacecraft with On-Off ActuatorsQinglei Hu. iasc, 17(3):343-354, 2011. [doi]
The following publications are possibly variants of this publication: