TECHNICAL PAPERS
Jul 1, 1998

Vibration Control of Flexible Manipulators Using Smart Structures

Publication: Journal of Aerospace Engineering
Volume 11, Issue 3

Abstract

The long reach robots required for space applications necessitate active vibration control algorithms for a better pointing performance. The inherent flexibility of the long and flexible space arms can generate undesirable vibrations, making their end-point controls very difficult, although they provide a large reach volume and payload capabilities. This paper presents a novel technique to control the vibrations of N modes of a flexible link attached to a rigid robot employing an Impedance Control Technique using piezo-ceramic actuators and fiber-optic sensors. A piezo-ceramic actuator model has been developed by considering the moments/forces generated by the piezo-ceramic actuator as nonconservative external forces. Successful simulation and experimental results have been obtained for vibration control of a cantilever beam which is attached to the end effector of the Titan-II robot arm.

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References

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Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 11Issue 3July 1998
Pages: 90 - 94

History

Published online: Jul 1, 1998
Published in print: Jul 1998

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Authors

Affiliations

S. Kalaycioglu
Canadian Space Agency, Spacecraft Engrg., 6767 Airport Rd., St-Hubert, Quebec, Canada J3Y 8Y9.
M. Giray
Canadian Space Agency, Spacecraft Engrg., 6767 Airport Rd., St-Hubert, Quebec, Canada J3Y 8Y9.
H. Asmer
Canadian Space Agency, Spacecraft Engrg., 6767 Airport Rd., St-Hubert, Quebec, Canada J3Y 8Y9.

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