Reference Model Variable Structure Output Feedback for Attitude Maneuvers Control of Flexible Spacecrafts

Qinglei Hu, Xiaozhi Gao, Guangfu Ma. Reference Model Variable Structure Output Feedback for Attitude Maneuvers Control of Flexible Spacecrafts. Intelligent Automation & Soft Computing, 15(1):53-62, 2009. [doi]

Abstract

Abstract is missing.