Vibration and stability control of robotic manipulator systems consisting of a thin-walled beam and a spinning tip rotor

Vibration and stability feedback control of a robotic manipulator modeled as a cantilevered thin-walled beam carrying a spinning rotor at its tip is investigated. The control is achieved via incorporation of adaptive capabilities that are provided by a system of piezoactuators, bonded or embedded into the host structure. Based on converse piezoelectric effect, the piezoactuators produce a localized strain field in response to an applied voltage, and as a result, an adaptive change of vibrational and stability response characteristics is obtained. A feedback control law relating the piezoelectrically induced bending moments at the beam tip with the appropriately selected kinematical response quantities is used, and the beneficial effects of this control methodology upon the closed-loop eigenvibration characteristics and stability boundaries are highlighted. The cantilevered structure modeled as a thin-walled beam, and built from a composite material, encompasses non-classical features, such as anisotropy, transverse shear, and secondary warping, and in this context, a special ply-angle configuration inducing a structural coupling between flapping-lagging and transverse shear is implemented. It is also shown that the directionality property of the material of the host structure used in conjunction with piezoelectric strain actuation capability, yields a dramatic enhancement of both the vibrational and stability behavior of the considered structural system. © 2002 Wiley Periodicals, Inc.

[1]  H. Tzou Piezoelectric Shells: Distributed Sensing and Control of Continua , 1993 .

[2]  Ohseop Song,et al.  On the static aeroelastic tailoring of composite aircraft swept wings modelled as thin-walled beam structures☆ , 1992 .

[3]  Ohseop Song,et al.  Synergistic implications of tailoring and adaptive materials technology on vibration control of anisotropic thin-walled beams , 2001 .

[4]  Leonard Meirovitch,et al.  Control of Cantilever Vibration via Structural Tailoring and Adaptive Materials , 1997 .

[5]  K. Yamanaka,et al.  The stability of a flexible link with a tip rotor and a compressive tip load , 1994, Proceedings of the 1994 IEEE International Conference on Robotics and Automation.

[6]  Ohseop Song,et al.  Adaptive vibrational behavior of cantilevered structures modeled as composite thin-walled beams , 1993 .

[7]  Liviu Librescu,et al.  Free Vibration Of Anisotropic Composite Thin-Walled Beams Of Closed Cross-Section Contour , 1993 .

[8]  Liviu Librescu,et al.  ANISOTROPY AND STRUCTURAL COUPLING ON VIBRATION AND INSTABILITY OF SPINNING THIN-WALLED BEAMS , 1997 .

[9]  P. Hughes Spacecraft Attitude Dynamics , 1986 .

[10]  L. Librescu,et al.  Integrated structural tailoring and control using adaptive materials for advanced aircraft wings , 1996 .

[11]  E. Smith,et al.  Formulation and evaluation of an analytical model for composite box-beams , 1991 .

[12]  Ohseop Song,et al.  VIBRATION AND STABILITY OF PRETWISTED SPINNING THIN-WALLED COMPOSITE BEAMS FEATURING BENDING–BENDING ELASTIC COUPLING , 2000 .

[13]  Liviu Librescu,et al.  Dynamic Response Control of Thin-Walled Beams to Blast Pulses Using Structural Tailoring and Piezoelectric Actuation , 1998 .

[14]  K. Yamanaka,et al.  The stability of a flexible link with a tip rotor and a compressive tip load , 1995, IEEE Trans. Robotics Autom..

[15]  Liviu Librescu,et al.  Static and Dynamic Validations of a Refined Thin-Walled Composite Beam Model , 2001 .