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检索条件"任意字段=Smart Structures and Materials 1994: Mathematics and Control in Smart Structures"

共 544 条记录，以下是231-240 订阅

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control of a hysteretic actuator using inverse hysteresis compensation.

Control of a hysteretic actuator using inverse hysteresis co...

引用

SPIE Conference on mathematics and control in smart structures

作者： Galinaitis, WS Rogers, RC Virginia Tech Dept Math Blacksburg VA 24061 USA

ISBN: (纸本)0819427675

The accurate control of a system that exhibits hysteresis requires a control strategy that incorporates some form of compensation for the hysteresis. One approach is to develop an accurate model P of the hysteresis and then use the inverse P-1 as a compensator (inverse compensation). This paper focuses on the problem of determining P and P-1 for a piezoelectric stack actuator. The KP operator (1) (2) is used to formulate the hysteresis operator P and from this an approximation P-m is derived. Compensation is then defined in terms of the inverse of the approximation, P-m(-1). Experimental data collected on an unloaded piezoelectric stack actuator is used to demonstrate the concept of inverse compensation. The parameters of P-m are identified using only major hysteresis loop data and results are given that show P-m provides an accurate model for both major and minor hysteresis loops. Results are then presented that demonstrate the capability of the inverse P-m(-1) to compensate for the actuator hysteresis.

关键词： hysteresis Preisach models inverse operators piezoelectric actuator

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Incorporating finite element techniques to simplify the impedance modeling of active structures

Incorporating finite element techniques to simplify the impe...

引用

SPIE Conference on mathematics and control in smart structures

作者： Fairweather, JA Craig, KC Rensselaer Polytech Inst Dept Mech Engn Aeronaut Engn & Mech Troy NY 12180 USA

ISBN: (纸本)0819427675

An impedance model(2) is formulated for the prediction of the response of structures to induced-strain actuation. The approach utilizes finite element analysis (FEA) to determine the host-structure mechanical impedance. The method couples this numerically obtained impedance to an analytical vibration solution of the induced-strain actuator to determine the dynamic response of the active structure. The methodology is demonstrated in the computation of the dynamic response of a beam structure to induced-strain actuation. This system has been extensively explored by the active structures community. Comparisons of the predicted dynamic response of this structure are made to the predictions of models previously documented in the literature. Experiments are conducted for the purpose of model validation, and an excellent agreement is demonstrated between die predictions of the FEA-based based impedance model and measurements made on physical systems. It is anticipated that the formulation extends the FEA-based impedance modeling approach to a broader class of active structures, those for which closed-form expressions of host-structure mechanical impedance are non-existent Use of the FEA-based impedance approach is suggested when modeling generic distributed structures possessing material anisotropy. mass loading, and non-uniform boundary conditions.

关键词： mechanical impedance active structure modeling beams plates finite elements

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Selective modal control of composite piezolaminated anisotropic shells

Selective modal control of composite piezolaminated anisotro...

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SPIE Conference on mathematics and control in smart structures

作者： Miller, SE Oshman, Y Abramovich, H Hughes Space & Commun El Segundo CA 90245 USA

ISBN: (纸本)0819427675

A general Selective Modal control (SMC) design methodology is presented for piezolaminated anisotropic shell systems which utilizes Selective Modal Transducers (SMT's) recently developed by the authors for piezo-shells in order to realize any number of possible modal control strategies. An SMC design procedure is specified which defines a step-by-step framework through which structural and control sub-design processes are effectively integrated, Several conditions which sufficiently ensure asymptotic stability are derived and then discussed in the context of deriving SMC methods which are stability robust to modeling and implementation errors. Several SMC examples are then given in which SMT's are designed and control laws chosen so as to allow for (1) the contributions of any given mode to the active energy extraction rate to be directly specified, (2) pole locations to be selectively and dynamically varied, or else (3) both pole locations and SMT design constants to be optimally determined. A numerical example is presented in which a stability-robust optimal SMC method is developed for a cantilevered anisotropic cylindrical shell panel. Maintaining a linear feedback law, a single self-sensing SMT is employed whose design parameters were chosen so as to optimize the system response to a given initial excitation. Frequency and transient response analyses show a dramatic enhancement in system performance and accurately concur with theoretical predictions. The example serves both to illustrate the design process and to independently validate SMT and SMC theoretical results as applied to shell systems characterized by aero-Gaussian curvature.

关键词： smart structures modal control modal transducers PVDF composites shells

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Vibration suppression of a skew cantilever plate using PZT patches

Vibration suppression of a skew cantilever plate using PZT p...

引用

SPIE Conference on mathematics and control in smart structures

作者： Pai, PF Rommel, B Naser, AS Schulz, MJ Univ Missouri Dept Mech & Aerosp Engn Columbia MO 65211 USA

ISBN: (纸本)0819427675

We investigate the control of steady-state vibrations of a cantilevered skew isotropic plate by using nonlinear saturation phenomena and PZT (lead zirconate titanate) patches as sensors and actuators. Modal testing and finite-element analysis are performed to study the bending-torsional dynamic characteristics due to the non-rectangular plate geometry. The control method uses linear second-order controllers coupled to the plate via quadratic terms to establish energy bridges between the plate and controllers. Each linear second-order controller is designed to have a 1:2 internal resonance with one of the plate vibration modes and hence is able to exchange energy with the plate at or around the specific modal frequency. Because of quadratic nonlinearities and 1:2 internal resonances, saturation phenomena exist and are used to suppress modal vibrations. To test this control technique in an efficient and systematic way, we built a digital control system that consists of SIMULINK modeling software and a dSPACE DS1102 controller in a pentium computer. Both numerical and experimental results show that this nonlinear control method is robust in suppression steady-state resonant vibrations without significant spill-over effects.

关键词： PZT actuator/sensor nonlinear controller skew plate active control

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Aeroservoelastic design with distributed actuation for high performance aircraft

Aeroservoelastic design with distributed actuation for high ...

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SPIE Conference on mathematics and control in smart structures

作者： Oz, H Ohio State Univ Columbus OH 43210 USA

ISBN: (纸本)0819427675

A new aeroelastic modal formulation in terms of real modal matrices and modal-state variables is introduced. Real biorthonormality relationships for aeroelastic modes are given with respect to structural matrices. The solution for distributed-parameter-control of an aeroelastic system is developed by modal synthesis from modal-state-space control inputs. in particular, the globally power optimal Independent Modal-Space control (IMSC) technique is used for maneuver (set-point) control of an aeroelastic system by a modal-performance-output synthesis approach. control power functionals for an aeroelastic system are defined for any actuation profile and control design. The known solution for the synthesized distributed-parameter closed-loop aeroelastic system is optimally approximated via a gain distribution error minimization technique integrating the transient and power performance characteristics of the system for implementation by distributed, spatially-discrete actuation profiles. For the same purpose, a Galerkin approximation is also given. The method is illustrated for a lifting surface simulating a wing to twist the win:: tip to a prescribed angle of attack by using different distributed actuation profiles. Various warped wing shapes can be affected by the approach by synthesizing through different selections of aeroelastic modes for control design resulting in different control power requirements.

关键词： aeroelasticity aeroservoelasticity IMSC modal control distributed-parameter-control control power optimal gain approximation wing shaping distributed actuation control non-self-adjoint system control

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Radiated noise control via structural vibration control

Radiated noise control via structural vibration control

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SPIE Conference on mathematics and control in smart structures

作者： Varadan, VV Gopinathan, SV Lim, YH Varadan, VK Penn State Univ Res Ctr Engn Elect & Acoust Mat University Pk PA 16802 USA

ISBN: (纸本)0819427675

Interior noise control in a cabin enclosure using active vibration control of the walls of the enclosure with discrete piezoelectric actuators and sensors is addressed. A hybrid approach using finite element formulation for the radiating walls of the enclosure. We use an exact 3D formulation without making the usual approximations for the electric field in the piezoelectric devices. The electrical boundary conditions and the charge on the electrodes are treated correctly Computational time is optimized by using plate elements for the structure and 3D element for the devices with transition elements to connect them. A PD-controller is used to relate the voltage output of the sensor in open circuit conditions to the charge input to the actuator via appropriate gains to control vibrations. The acoustic part of the problem is modeled via a modal approach The modal representation of the pressure is used as a mechanical force term on the structure which can be written in terms of a virtual mass. The driving term for the acoustic field is in turn the displacements on the surface of the radiating walls which is computed from the structural equations. This accounts for the acoustic field-structure interaction and the equations are solved simultaneously. By adjusting the feedback gain, significant noise reduction is achieved globally within the cavity for the dominant vibrational modes of the radiating panel.

关键词： Sensors Actuators Acoustics Vibration control Chemical elements Feedback control Electrodes Active vibration control Gadolinium Transition metals

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Generalized dissipation in hysteretic systems

Generalized dissipation in hysteretic systems

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IEEE Conference on Decision and control

作者： R.B. Gorbet K.A. Morris Department of Electrical Engineering University of Toronto Toronto ONT Canada Department of Applied Mathematics University of Waterloo Waterloo ONT Canada

We give a formal definition of dissipative systems that is considerably more general than earlier definitions. The measured output is irrelevant in this formulation. The key component of dissipation is an appropriate work rate. We also define cycle-dissipation and show how it can be used to obtain a suitable work rate. Using this idea, we propose a new work rate for the Preisach hysteresis model, and demonstrate dissipativity with respect to this rate. The Preisach model describes the dynamics of many "smart materials" such as shape memory alloys. This new type of dissipativity will be beneficial in the design of position controllers for SMA.

关键词： control systems Shape memory alloys Flexible structures Shape control Force control Robust control Magnetic hysteresis Magnetic materials Piezoelectric materials Nonlinear control systems

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smart structures and materials 1997: mathematics and control in smart structures

Smart Structures and Materials 1997: Mathematics and Control...

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smart structures and materials 1997: mathematics and control in smart structures

The proceedings contains 69 papers. Following topics are discussed: shape memory alloys;control theory;finite element modeling;electrically/magnetically active materials;and active devices - modeling.

ISBN: (纸本)0819424528

关键词： Intelligent structures

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Aeroelastic control using smart structures and acceleration feedback

Aeroelastic control using smart structures and acceleration ...

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smart structures and materials 1997: mathematics and control in smart structures

作者： Yedavalli, Rama K. Tseng, Yuan-Wei Khot, Narendra S. Veley, Duane E. The Ohio State Univ. Columbus OH USA

ISBN: (纸本)0819424528

In this paper, a design approach for controlling a composite plate structure subject to aeroelastic loading using piezoelectric actuators and sensors is presented. The nature of the sensing variables is exploited and accommodated in the control design algorithm. The controller is a feedback controller that uses various measurements related to motion variables such as accelerations, velocities and displacements. Proposed controller designs in this paper are based on equivalent first order state-space baseline design gains that use existing control system design software. The proposed method provides different norms for controller gains, thereby allowing more flexibility in gain magnitudes and selection of sensors and still meet the time response specifications.

关键词： Intelligent structures

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Vibration and tracking control of piezoceramic-based smart structures via quantitative feedback theory

Vibration and tracking control of piezoceramic-based smart s...

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smart structures and materials 1997: mathematics and control in smart structures

作者： Choi, Seung-Bok Cho, Seung-Sang Jeon, Young-Sik Inha Univ. Incheon South Korea

ISBN: (纸本)0819424528

This paper presents robust vibration and position tracking control of a flexible smart structure featuring a piezoceramic actuator. A cantilever beam structure with a surface-bonded piezoceramic actuator is proposed, and its governing equation of motion and associated boundary conditions are derived from Hamilton's principle. The transfer function from control input voltage to output displacement is then established in Laplace domain in order to formulate a robust controller using the quantitative feedback theory (QFT). A robust QFT compensator is designed on the basis of a stability criterion which prescribes a bound on the peak value of an M-contour in the Nichols chart. In the formulation of the compensator, disturbance rejection specification and tracking performance bounds are specified to guarantee the robustness of the system to plant uncertainties and external disturbances. A prefilter is also designed for the improvement of step and sinusoidal tracking control performances. Vibration and position tracking control performances are evaluated through computer simulation and experimental implementation in order to demonstrate the efficiency and robustness of the proposed control methodology.

关键词： Vibration control

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