mechatronics dynamics of electromechanical and piezoelectric systems pdf

www.EngineeringBooksPDF.com SOLID MECHANICS AND ITS APPLICATIONS Volume 136 Series Editor: G.M.L GLADWELL Department of Civil Engineering University of Waterloo Waterloo, Ontario, Canada N2L 3GI Aims and Scope of the Series The fundamental questions arising in mechanics are: Why?, How?, and How much? The aim of this series is to provide lucid accounts written by authoritative researchers giving vision and insight in answering these questions on the subject of mechanics as it relates to solids The scope of the series covers the entire spectrum of solid mechanics Thus it includes the foundation of mechanics; variational formulations; computational mechanics; statics, kinematics and dynamics of rigid and elastic bodies: vibrations of solids and structures; dynamical systems and chaos; the theories of elasticity, plasticity and viscoelasticity; composite materials; rods, beams, shells and membranes; structural control and stability; soils, rocks and geomechanics; fracture; tribology; experimental mechanics; biomechanics and machine design The median level of presentation is the first year graduate student Some texts are monographs defining the current state of the field; others are accessible to final year undergraduates; but essentially the emphasis is on readability and clarity For a list of related mechanics titles, see final pages www.EngineeringBooksPDF.com Mechatronics Dynamics of Electromechanical and Piezoelectric Systems by A PREUMONT ULB Active Structures Laboratory, Brussels, Belgium www.EngineeringBooksPDF.com A C.I.P Catalogue record for this book is available from the Library of Congress ISBN-10 ISBN-13 ISBN-10 ISBN-13 1-4020-4695-2 (HB) 978-1-4020-4695-7 (HB) 1-4020-4696-0 (e-book) 978-1-4020-4696-4 (e-book) Published by Springer, P.O Box 17, 3300 AA Dordrecht, The Netherlands www.springer.com Printed on acid-free paper All Rights Reserved © 2006 Springer No part of this work may be reproduced, stored in a retrieval system, or transmitted in any form or by any means, electronic, mechanical, photocopying, microfilming, recording or otherwise, without written permission from the Publisher, with the exception of any material supplied specifically for the purpose of being entered and executed on a computer system, for exclusive use by the purchaser of the work Printed in the Netherlands www.EngineeringBooksPDF.com ” Tenez, mon ami, si vous y pensez bien, vous trouverez qu’en tout, notre v´eritable sentiment n’est pas celui dans lequel nous n’avons jamais vacill´e; mais celui auquel nous sommes le plus habituellement revenus.” Diderot, (Entretien entre D’Alembert et Diderot) www.EngineeringBooksPDF.com Contents Preface xiii Lagrangian dynamics of mechanical systems 1.1 Introduction 1.2 Kinetic state functions 1.3 Generalized coordinates, kinematic constraints 1.3.1 Virtual displacements 1.4 The principle of virtual work 1.5 D’Alembert’s principle 1.6 Hamilton’s principle 1.6.1 Lateral vibration of a beam 1.7 Lagrange’s equations 1.7.1 Vibration of a linear, non-gyroscopic, discrete system 1.7.2 Dissipation function 1.7.3 Example 1: Pendulum with a sliding mass 1.7.4 Example 2: Rotating pendulum 1.7.5 Example 3: Rotating spring mass system 1.7.6 Example 4: Gyroscopic effects 1.8 Lagrange’s equations with constraints 1.9 Conservation laws 1.9.1 Jacobi integral 1.9.2 Ignorable coordinate 1.9.3 Example: The spherical pendulum 1.10 More on continuous systems 1.10.1 Rayleigh-Ritz method 1.10.2 General continuous system 1.10.3 Green strain tensor 1.10.4 Geometric strain energy due to prestress 1.10.5 Lateral vibration of a beam with axial loads vii www.EngineeringBooksPDF.com 1 10 11 14 17 19 19 20 22 23 24 27 29 29 30 32 32 32 34 34 35 37 viii Contents 1.10.6 Example: Simply supported beam in compression 38 1.11 References 39 Dynamics of electrical networks 2.1 Introduction 2.2 Constitutive equations for circuit elements 2.2.1 The Capacitor 2.2.2 The Inductor 2.2.3 Voltage and current sources 2.3 Kirchhoff’s laws 2.4 Hamilton’s principle for electrical networks 2.4.1 Hamilton’s principle, charge formulation 2.4.2 Hamilton’s principle, flux linkage formulation 2.4.3 Discussion 2.5 Lagrange’s equations 2.5.1 Lagrange’s equations, charge formulation 2.5.2 Lagrange’s equations, flux linkage formulation 2.5.3 Example 2.5.4 Example 2.6 References 41 41 42 42 43 45 46 47 48 49 51 53 53 54 54 57 59 Electromechanical s ystems 3.1 Introduction 3.2 Constitutive relations for transducers 3.2.1 Movable-plate capacitor 3.2.2 Movable-core inductor 3.2.3 Moving-coil transducer 3.3 Hamilton’s principle 3.3.1 Displacement and charge formulation 3.3.2 Displacement and flux linkage formulation 3.4 Lagrange’s equations 3.4.1 Displacement and charge formulation 3.4.2 Displacement and flux linkage formulation 3.4.3 Dissipation function 3.5 Examples 3.5.1 Electromagnetic plunger 3.5.2 Electromagnetic loudspeaker 3.5.3 Capacitive microphone 3.5.4 Proof-mass actuator 3.5.5 Electrodynamic isolator 61 61 61 62 65 68 71 71 72 73 73 73 74 76 76 77 79 82 84 www.EngineeringBooksPDF.com Contents 3.5.6 The Sky-hook damper 3.5.7 Geophone 3.5.8 One-axis magnetic suspension 3.6 General electromechanical transducer 3.6.1 Constitutive equations 3.6.2 Self-sensing 3.7 References ix 86 87 89 92 92 93 94 Piezoelectric systems 95 4.1 Introduction 95 4.2 Piezoelectric transducer 96 4.3 Constitutive relations of a discrete transducer 99 4.3.1 Interpretation of k2 103 4.4 Structure with a discrete piezoelectric transducer 105 4.4.1 Voltage source 107 4.4.2 Current source 107 4.4.3 Admittance of the piezoelectric transducer 108 4.4.4 Prestressed transducer 109 4.4.5 Active enhancement of the electromechanical coupling111 4.5 Multiple transducer systems 113 4.6 General piezoelectric structure 114 4.7 Piezoelectric material 116 4.7.1 Constitutive relations 116 4.7.2 Coenergy density function 118 4.8 Hamilton’s principle 121 4.9 Rosen’s piezoelectric transformer 124 4.10 References 130 Piezoelectric laminates 5.1 Piezoelectric beam actuator 5.1.1 Hamilton’s principle 5.1.2 Piezoelectric loads 5.2 Laminar sensor 5.2.1 Current and charge amplifiers 5.2.2 Distributed sensor output 5.2.3 Charge amplifier dynamics 5.3 Spatial modal filters 5.3.1 Modal actuator 5.3.2 Modal sensor www.EngineeringBooksPDF.com 131 131 131 133 136 136 136 138 139 139 140 x Contents 5.4 Active beam with collocated actuator-sensor 5.4.1 Frequency response function 5.4.2 Pole-zero pattern 5.4.3 Modal truncation 5.5 Piezoelectric laminate 5.5.1 Two dimensional constitutive equations 5.5.2 Kirchhoff theory 5.5.3 Stiffness matrix of a multi-layer elastic laminate 5.5.4 Multi-layer laminate with a piezoelectric layer 5.5.5 Equivalent piezoelectric loads 5.5.6 Sensor output 5.5.7 Remarks 5.6 References Active and passive damping with piezoelectric transducers 6.1 Introduction 6.2 Active strut, open-loop FRF 6.3 Active damping via IFF 6.3.1 Voltage control 6.3.2 Modal coordinates 6.3.3 Current control 6.4 Admittance of the piezoelectric transducer 6.5 Damping via resistive shunting 6.5.1 Damping enhancement via negative capacitance shunting 6.5.2 Generalized electromechanical coupling factor 6.6 Inductive shunting 6.6.1 Alternative formulation 6.7 Decentralized control 6.8 General piezoelectric structure 6.9 Self-sensing 6.9.1 Force sensing 6.9.2 Displacement sensing 6.9.3 Transfer function 6.10 Other active damping strategies 6.10.1 Lead control 6.10.2 Positive Position Feedback (PPF) www.EngineeringBooksPDF.com 141 142 143 145 147 148 148 149 151 152 153 154 156 159 159 161 165 165 167 169 170 172 175 176 176 181 183 184 185 186 187 187 191 191 192 Contents xi 6.11 Remark 195 6.12 References 195 Bibliography 199 Index 205 www.EngineeringBooksPDF.com 6.10 Other active damping strategies 191 to G(0) > Thus, if C3 = C, G(s) exhibits alternating poles and zeros on the imaginary axis, starting with a zero, while if C3 = C(1 − k2 ), it starts with a pole This is illustrated in Fig.6.14 which shows the effect of C3 on a typical open-loop FRF (this figure has been generated with the following data: ω1 = 1, ω2 = 2, ω3 = 3, ν1 = ν2 = ν3 = 0.2, k = 0.5, r = 1, and a uniform damping ξi = 0.01) 6.10 Other active damping strategies In Fig.6.14, all the FRF exhibit alternating poles and zeros; however, they differ in the way the pole-zero pattern starts at low frequency The FRF corresponding to C3 = C starts with a low frequency zero and is identical to that of Fig.6.4(a) or Fig.6.5(b); the IFF is a very effective control strategy for this situation On the other hand, for C3 = C(1 − k2 ), the FRF starts with a low frequency pole, and the IFF strategy would be unstable for this pole-zero configuration; alternative strategies applicable in this case are discussed below 6.10.1 Lead control The first case to consider is that where the open-loop FRF exhibits some roll-off at high frequency, usually −40 dB/decade, corresponding to the open-loop transfer function having two poles in excess of zeros (decays as ω −2 at high frequency) The modal expansion of the open-loop transfer function is n bT φi φTi b G(s) = (6.128) µ (s2 + ωi ) i=1 i This corresponds typically to the case of a point force actuator collocated with a displacement sensor The pole-zero pattern is that of Fig.6.15; this system can be damped with a lead compensator : H(s) = g s+z s+p (p ≫ z) (6.129) The block diagram of the control system is shown in Fig.6.16 This controller takes its name from the fact that it produces a phase lead in the frequency band between z and p, bringing active damping to all the modes belonging to z < ωi < p All the branches of the root locus belong to the left-half plane, which means that the closed-loop system has guaranteed stability, at least if perfect actuator and sensor dynamics are assumed www.EngineeringBooksPDF.com 192 Active and passive damping with piezoelectric transducers Im(s) jz i j! i àp Lead Structure Re(s) àz Fig 6.15 Root locus of the lead compensator applied to a structure with collocated actuator and sensor (open-loop transfer function with two poles in excess of zeros) The controller does not have any roll-off, but the roll-off of the structure is enough to guarantee gain stability at high frequency + g s+z s+p u G(s) = P i (b Tỵ i) i(s 2+! 2i ) y Fig 6.16 Block diagram of the lead compensator applied to a structure with collocated actuator and sensor (open-loop transfer function with two poles in excess of zeros) 6.10.2 Positive Position Feedback (PPF) The situation where the open-loop FRF has a roll-off of -40 dB/decade is not the most frequent one when piezoelectric actuators are used Figure 5.10 shows a typical experimental open-loop FRF corresponding to an active cantilever beam with collocated PZT actuator and sensor patches, similar to that of Fig.5.6 As observed earlier, this open-loop FRF does not roll-off at high frequency, and this was attributed to a feedthrough term in the system equation; a similar situation occurs in (6.125) When www.EngineeringBooksPDF.com 6.10 Other active damping strategies 193 the open-loop transfer function has a feedtrough component, the system stability requires that the compensator includes some roll-off.4 The Positive Position Feedback was proposed (Goh & Caughey, 1985, Fanson & Caughey, 1990) to achieve just that, for systems similar to that of Fig.5.6 The controller consists of a second order filter H(s) = s2 −g + 2ξf ωf s + ωf2 (6.130) where the damping ξf is usually high (0.5 to 0.7), and the filter frequency ωf is adapted to target a specific mode The block diagram of the control system is shown in Fig.6.17; the negative sign in H(s), which produces a positive feedback, is the origin of the name of this controller + àg f! f+! f s 2+2ứ u G(s) = P i (b Tỵ i) ö i(s 2+! 2i ) y Fig 6.17 Block diagram of the PPF controller applied to a structure with collocated actuator and sensor (the open-loop transfer function has the same number of poles and zeros) Figure 6.18 shows typical root loci when the PPF poles are targeted to mode and mode 2, respectively (i.e ωf close to ω1 or ω2 , respectively) One sees that the whole locus is contained in the left half plane, except one part on the positive real axis, but that part of the locus is reached only for large values of g, which are not used in practice The stability condition can be established as follows: the characteristic equation of the closed loop system reads ψ(s) = + gH(s)G(s) = − n bT φi φTi b g }=0 { 2 s + 2ξf ωf s + ωf i=1 µi (s2 + ωi ) or n ψ(s) = s2 + 2ξf ωf s + ωf2 − g{ i=1 bT φi φTi b }=0 µi (s2 + ωi ) According to the Routh-Hurwitz criterion for stability, if one of the in the IFF control discussed earlier, there is a feedthrough in G(s), but the controller 1/s has a -20 dB/decade roll-off www.EngineeringBooksPDF.com 194 Active and passive damping with piezoelectric transducers co efficients of the power expansion of the characteristic equation becomes negative, the system is unstable It is not possible to write the power expansion ψ(s) explicitly for an arbitrary value of n, however, one can see easily that the constant term (in s0 ) is n an = ψ(0) = ωf2 − g i=1 bT φi φTi b µi ωi In this case, an becomes negative when the static loop gain becomes larger than The stability condition is therefore gG(0)H(0) = g n bT φi φTi b }