2,953 research outputs found
High speed, precision motion strategies for lightweight structures
Research on space telerobotics is summarized. Adaptive control experiments on the Robotic Arm, Large and Flexible (RALF) were preformed and are documented, along with a joint controller design for the Small Articulated Manipulator (SAM), which is mounted on the RALF. A control algorithm is described as a robust decentralized adaptive control based on a bounded uncertainty approach. Dynamic interactions between SAM and RALF are examined. Unstability of the manipulator is studied from the perspective that the inertial forces generated could actually be used to more rapidly damp out the flexible manipulator's vibration. Currently being studied is the modeling of the constrained dynamics of flexible arms
Invited Review: Recent developments in vibration control of building and bridge structures
This paper presents a state-of-the-art review of recent articles published on active, passive, semi-active and hybrid vibration control systems for structures under dynamic loadings primarily since 2013. Active control systems include active mass dampers, active tuned mass dampers, distributed mass dampers, and active tendon control. Passive systems include tuned mass dampers (TMD), particle TMD, tuned liquid particle damper, tuned liquid column damper (TLCD), eddy-current TMD, tuned mass generator, tuned-inerter dampers, magnetic negative stiffness device, resetting passive stiffness damper, re-entering shape memory alloy damper, viscous wall dampers, viscoelastic dampers, and friction dampers. Semi-active systems include tuned liquid damper with floating roof, resettable variable stiffness TMD, variable friction dampers, semi-active TMD, magnetorheological dampers, leverage-type stiffness controllable mass damper, semi-active friction tendon. Hybrid systems include shape memory alloys-liquid column damper, shape memory alloy-based damper, and TMD-high damping rubber
Review of Suspension Control and Simulation of Passive, Semi-Active and Active Suspension Systems Using Quarter Vehicle Model
This paper reviewed vehicle suspension control and also simulated passive, semi-active and active suspension system using quarter vehicle model with the help of Matlab software. The suspension system of a vehicle is meant to isolate the occupants of the vehicle from the disturbances occasioned by irregular road surface to improve ride quality. The main essence of this work is to review and assess the effectiveness of the vehicle suspension system by comparing the ride quality of passive, semi active and active suspension systems based on the set parameters. These parameters are: the unsprang mass displacement, sprung mass displacement and the suspension deflection. When the unsprung mass displacement and the sprung mass displacement were compared, it was found that, the passive suspension system has the highest magnitudes of both unsprung mass and sprung mass displacements. The active suspension system has the least unsprung mass and sprung mass displacements magnitudes. Based on these two parameters that were compared, it was therefore convenient to conclude that the active suspension system provides the best ride quality than the passive and semi-active suspension systems. The semi-active suspension system was also found to provide better ride quality than the passive suspension system based on unsprung mass and sprung mass displacements. When the suspension deflections of the passive, semi-active and active suspension systems were compared, it was found that, the semi-active suspension system has the least suspension deflection than the passive and active suspension systems under the same road conditions
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Όλ¬Έ (λ°μ¬) -- μμΈλνκ΅ λνμ : 곡과λν κΈ°κ³κ³΅νκ³Ό, 2020. 8. μ‘°λ§Ήν¨.Model updating methods for structural systems have been introduced in various numerical processes. To improve the updating method, the process must require an accurate analysis and minimized experimental uncertainties. Finite element model was employed to describe structural system. Structural vibration behavior of a plate model is expressed as a combination of the initial state behavior of the structure and its associated perturbations. The dynamic behavior obtained from a limited number of accessible nodes and their associated degrees of freedom is employed to detect structural changes that are consistent with the perturbations. The equilibrium model is described in terms of the measured and unmeasured modal data. Unmeasured information is estimated using an iterated improved reduction scheme. Because the identification problem depends on the measured information, the quality of the measured data determines the accuracy of the identified model and the convergence of the identification problem. The accuracy of the identification depends on the measurement/sensor location. We propose a more accurate identification method using the optimal sensor location selection method. Experimental examples are adopted to examine the convergence and accuracy of the proposed method applied to an inverse problem of system identification. Model updating methods for structural systems have been introduced in various fields. Model updating processes are important for improving a models accuracy by considering experimental data. Structural system identification was achieved here by applying the degree of freedom-based reduction method and the inverse perturbation method. Experimental data were obtained using the specific sensor location selection method. Experimental vibration data were restored to a full finite element model using the reduction method to compare and update the numerical model. Applied iteratively, the improved reduced system method boosts model accuracy
during full model restoration; however, iterative processes are time-consuming. The calculation efficiency was improved using the system equivalent reduction-expansion process in concert with the proper orthogonal
decomposition. A convolutional neural network was trained and applied to the updating process. We propose the use of an efficient model updating method using a convolutional neural network to reduce calculation time. Experimental and numerical examples were adopted to examine the efficiency and accuracy of the model updating method using a convolutional neural network. A more complex model is applied for model updating method and validated with proposed methods. A bolt assembly modeling is introduced and simplified with verified methodologies.ꡬ쑰 μμ€ν
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νκ³ μ€νμ ν΅ν λͺ¨λΈ κ°±μ μΌλ‘ λμ± λ¨μνλ λͺ¨λΈλ§μ μ μν©λλ€.Chapter 1. Introduction 1
1.1 Frequency model updating method . 1
1.2 Reduction methods . 3
1.2.1 Degree of freedom-based reduction method 3
1.2.2 Iterated improved reduced system 4
1.2.3 Proper orthogonal decomposition 8
1.2.4 System equivalent reduction-expansion process 9
1.3 Structural system identification . 11
1.3.1 Balance equation for system identification . 15
1.3.2 Inverse perturbation method . 16
1.4 Machine learning in identification process . 20
Chapter 2. Sensor location selection method 21
2.1 Vibration test setup . 21
2.1.1 Vibration test setup for system identification 21
2.1.2 Vibration data rebuilt for in-house code . 22
2.2 Nodal point consideration . 26
2.2.1 Sequential elimination method 26
2.2.2 Energy method 27
2.2.3 Nodal point consideration 28
2.2.4 Numerical examples . 28
2.3 Sensor location selection method 32
Chapter 3. Residual error equation for identificataion process 36
3.1 Parameter optimizing equation setup 36
3.2 Convergence criterion . 38
3.3 Weighting factor for parameter evaluation 39
3.4 Identification examples 42
Chapter 4. Convolutional neural networks-based system identification method 54
4.1 Introduction . 54
4.2 The balance equation of the model updating method . 57
4.2.1 The IPM method 58
4.2.2 The DOF-based reduction method 59
4.2.3 Experimental data for the model updating method 63
4.3 Convolutional neural network-based identification 67
4.3.1 The SEREP and POD . 67
4.3.2 The 2D-CNN 72
4.4 Experimental examples 77
Chapter 5. A model updating of complex models 94
5.1 The model updating and digital twin . 94
5.2 A complex model example 95
5.2.1 The tank bracket model 95
5.2.2 The sensor location selection 98
5.3 The bolt joint assembly simplification . 102
Chapter 6. Conclusion 109
Appendix A. Structural design of soft robotics using a joint structure of photo responsive polymers 113
A.1 Overview 113
A.2 Structural desing of soft robotics . 114
A.3 Experimental setup 117
A.3.1 Systhesis process 117
A.3.2 Sample preparation 118
A.3.3 Spectrometer characterization 118
A.4 Structural modeling . 121
A.4.1 Multiscale mechanincs 121
A.4.2 Nonlinear FEM with a co-rotational formulation 123
A.5 Results and discussion 128
A.6 Summary of Appendix A 142
Bibliography 145
Abstract in Korean 158Docto
A Supervisor for Control of Mode-switch Process
Many processes operate only around a limited number of operation points. In order to have adequate control around each operation point, and adaptive controller could be used. When the operation point changes often, a large number of parameters would have to be adapted over and over again. This makes application of conventional adaptive control unattractive, which is more suited for processes with slowly changing parameters. Furthermore, continuous adaptation is not always needed or desired. An extension of adaptive control is presented, in which for each operation point the process behaviour can be stored in a memory, retrieved from it and evaluated. These functions are co-ordinated by a ΒΏsupervisorΒΏ. This concept is referred to as a supervisor for control of mode-switch processes. It leads to an adaptive control structure which quickly adjusts the controller parameters based on retrieval of old information, without the need to fully relearn each time. This approach has been tested on experimental set-ups of a flexible beam and of a flexible two-link robot arm, but it is directly applicable to other processes, for instance, in the (petro) chemical industry
Structural dynamics branch research and accomplishments for fiscal year 1987
This publication contains a collection of fiscal year 1987 research highlights from the Structural Dynamics Branch at NASA Lewis Research Center. Highlights from the branch's four major work areas, Aeroelasticity, Vibration Control, Dynamic Systems, and Computational Structural Methods, are included in the report as well as a complete listing of the FY87 branch publications
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