Flexible Manipulator Control Based on Singular Perturbation Theory Study

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Abstract:

Aiming at the problem of tracking the reference trajectory and suppressing the beam vibration for flexible manipulator, this paper separated the system of flexible-link manipulator into slow subsystem and fast subsystem two different time scale subsystems based on singular perturbation theory and proposes a simple composite control algorithm. For the slow subsystem, a sliding mode controller is employed to track the desired trajectory, while optimal controller is used to stabilize the fast subsystem to suppress the vibration. Finally, the simulation results demonstrate the good performance of the proposed control strategy.

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69-73

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August 2013

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© 2013 Trans Tech Publications Ltd. All Rights Reserved

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[1] Chen Zhi-yong Chen Li. Adaptive variable structure control for flexible space manipulator based on hybrid sliding mode concept[J]. Engineering Mechanics, 2012, 29(2): 216-221.

Google Scholar

[2] Dang Jin, Ni Fenglei, Liu Yechao, Liu Hong. Control strategy for flexible manipulator based on feedforward compensation and Fuzzy-sliding mode control. [J]. Journal of xi'an jiaotong university, 2011, 45(3): 75-80.

DOI: 10.1109/icma.2012.6285106

Google Scholar

[3] Peng Jigen, Ni Yuanhua, Qiao Hong. Neural network control of flexible-joint robot manipulator[J]. Acta automatica sinica, 2007, 33(2): 175-180.

DOI: 10.1360/aas-007-0175

Google Scholar

[4] Liu Huaping, Sun Fuchun, He Kezhong, Sun Zengqi. Survey of singularly perturbaed control system: theory and applications[J]. Control theory and applications. 2003, 20(1): 1-7.

DOI: 10.1109/cdc.2003.1272469

Google Scholar

[5] Mohamed W. Mehrez, Ayman A. EI-Badawy. Effect of the joint inetia on selection of under-actuated control algorithm for flexible-link manipulators. Mechanism and Machine Theory. 2010(45): 967-980.

DOI: 10.1016/j.mechmachtheory.2010.03.003

Google Scholar

[6] Q.L. Hu. Sliding mode attitude control with L2 -gain performance and vibration reduction of flexible spacecraft with actuator dynamics[J]. Acta Astronautica, 2010(67): 572-583.

DOI: 10.1016/j.actaastro.2010.04.018

Google Scholar