Proceedings of the 16th ASIA PACIFIC VIBRATION CONFERENCE

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Proceedings of the 16th
ASIA PACIFIC VIBRATION CONFERENCE
Edited by:
Yoshihiro Narita, Nguyen Van Khang, and Nguyen Quang Hoang
Organized by:
Vietnam Association of Mechanics (VAM)
Hanoi University of Science and Technology (HUST)
Bachkhoa Publishing House, Hanoi 2015
Proceedings of the 16th
ASIA PACIFIC VIBRATION CONFERENCE
24-26 November, 2015
Hanoi, Vietnam
Edited by:
Prof. Yoshihiro Narita (Hokkaido University, Japan)
Prof. Nguyen Van Khang (Hanoi University of Science and Technology, Vietnam)
Dr. Nguyen Quang Hoang (Hanoi University of Science and Technology, Vietnam)
Organized by:
Vietnam Association of Mechanics (VAM)
Hanoi University of Science and Technology (HUST)
Bachkhoa Publishing House, Hanoi 2015
16th Asia Pacific Vibration Conference
24-26 November, 2015
HUST, Hanoi, Vietnam
APVC2015
International Organizing Committee
Chairman
Yoshihiro Narita (Hokkaido University, Japan)
Members
Shigehiko Kaneko (University of Tokyo, Japan)
Andy C.C. Tan (Queensland University of Technology, Australia)
Nong Zhang (University of Technology, Sydney, Australia)
Athol J. Carr (University of Canterbury, New Zealand)
Hong Hee Yoo (Hanyang University, Korea)
Youngjin Park (KAIST, Korea)
M. Salman Leong (University of Technology, Malaysia)
R. Abdul Rahman (University of Technology, Malaysia)
Li Cheng (Hong Kong Polytechnic University, Hong Kong)
Takuya Yoshimura (Tokyo Metropolitan University, Japan)
Yi Min Zhang (Northeastern University, China)
Zhi Chao Hou (Tsinghua University, China)
Nguyen Van Khang (Hanoi University of Science and Technology, Vietnam)
Honorable Advisory Board
Dr. Nguyen Quan (Minister, Ministry of Science and Technology)
Prof. Duong Ngoc Hai (Vice-President, Vietnam Academy of Science and Technology)
Dr. Tran Viet Hung (Vice-President, Vietnam Union of Science and Technology Association)
Prof. Nguyen Hoa Thinh (President, Vietnam Association of Mechanics)
Local Programming Committee
Chairman
Nguyen Van Khang (HUST, Hanoi)
Members
Nguyen Dong Anh (IMECH, Hanoi),
Dao Huy Bich (VNU, Hanoi)
Nguyen Phong Dien (HUST, Hanoi)
Nguyen Dinh Duc (VNU, Hanoi)
Nguyen Dung (IAMI, Hochiminh City)
Hoang Ha (Ministry of Transport, Hanoi)
Pham Duy Hoa (University of Civil Engineering, Hanoi)
Nguyen Tien Khiem (IMECH, Hanoi)
Vu Van Khiem (MOST, Hochiminh City)
Ngo Kieu Nhi (HCMUT, Hochiminh City)
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Dinh Van Phong (HUST, Hanoi)
Do Kien Quoc (HCMUT, Hochiminh City)
Nguyen Chi Sang (NARIME, Hanoi)
Do Sanh (HUST, Hanoi)
Le Luong Tai (Thai Nguyen University, Thainguyen)
Tran Ich Thinh (HUST, Hanoi)
Local Organizing Committee
Co-Chairs
Nguyen Phong Dien, Dinh Van Phong (HUST)
Members
Pham Thanh Chung (HUST, Hanoi)
Hoang Manh Cuong (Maritime University, Haiphong)
Nguyen Van Du (Thai Nguyen University, Thainguyen)
Le Thai Hoa (VNU, Hanoi)
Trieu Quoc Loc (National Ins. Labour Protection, Hanoi)
Phan Dang Phong (NARIME, Hanoi)
Nguyen Trong Phuoc (HCMUT, Hochiminh City)
Nguyen Minh Phuong (HUST, Hanoi)
Nguyen Van Quyen (HUST, Hanoi)
Tran Dinh Son (University Mining and Geology, Hanoi)
Nguyen Xuan Thanh (University of Civil Engineering, Hanoi)
Nguyen Xuan Toan (DUT, Danang)
La Duc Viet (IMECH, Hanoi)
Conference location
Hanoi University of Science and Technology
1 Dai Co Viet Road, Hanoi, Vietnam
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CONTENTS
Section A. Vibration of Continuous Systems and Structural Dynamics
Sound Projection and Capture
Semyung Wang, Kihyun Kim and Homin Ryu
1
Study on power generation with in-flow fluidelastic instability
Tomomichi Nakamura, Takuya Sumitani and Joji Yamada
6
Overall Stiffness Identification of Short – Span Bridges Based on Change in Representative
Power Spectral Density
Kieu Nhi – NGO, QuangThanh – NGUYEN, BaoToan – PHAM, Da Thao – NGUYEN
Proposing a New Feature of Short – Span Bridges under Real Traffic for Damage Dectection
KieuNhi-Ngo, BaoToan-Pham, QuangThanh-Nguyen
Study the effects of applied tension and position of “cap magnets” on self-oscillating frequency of a taut
membrane under aerodynamic load
VU Dinh Quy
13
21
28
Dynamic Behavior of Cantilever Beam with Slightly Gapped Support under Random Excitation
Shozo Kawamura, Kyosuke Imamura, Masami Matsubara
32
Linear density identification of beams with free-free boundary condition
Masami Matsubara, Akihiro Aono, Shozo Kawamura
37
A Wavelet-decomposed Semi-analytical Model for Flexural Vibration of a Beam with Acoustic
Black Hole Effect
Liling TANG, Su ZHANG, Hongli JI, Jinhao QIU and Li CHENG
42
Vibration analysis of a rotating blade composed of functionally graded materials
Yutaek Oh, Hong Hee Yoo
50
Evaluation of damping properties of damping beam with natural rubber/cellulose composites
Masami Matsubara, Shozo Kawamura, Asahiro Nagatani, Nobutaka Tsujiuchi, Akihito Ito
54
Finite element analysis of APR1400 nuclear reactor
Jong-beom Park, No-Cheol Park, Sang Jeong Lee, Woo-Jin Roh
59
Vibration and stability analysis of functionally graded carbon nanotube-reinforced composite beams
immersed in axial pulsating fluid
Hossein Hemmati, Hassan Nahvi
63
Benchmark Test Function for Assessing the Lay-up Optimization Methods in Plate Vibration
Toshiya Hayashi, Shinya Honda, Yoshihiro Narita
69
Free Vibration Analysis of Cantilevered Symmetrically laminated Plates with Attached Mass
Kenji Hosokawa, Tatsuro Ohashi
77
An experimental study on anechoic vibrations of a beam with wedge-shape and damping treatment
Soon-woo Seo, Kwang-joon Kim
81
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Vibration optimization of composite sandwich plate with soft core by using refined zigzag theory
Shinya Honda, Takahito Kumagai, Yoshihiro Narita
Smoothed particle hydrodynamics simulation of aquatic propulsion mechanism by using vibrating
elastic plate
Masashi Sasuga, Hirosuke Horii, Nobuyuki Furuya, Yuichi Matsumura, Kohei Furuya
Vibration Analysis of a Floating Platform for an Offshore Wind Turbine
Joong Hyeok Lee, Jin Ho Ahn, Jun Ho Byun, Byeonghee Kim, and Seockhyun Kim
87
93
99
Study on Seismic Evaluation System of Elevator Rope
Yuta Shimura,Satoshi Fujita, Keisuke Minagawa
103
Development of Escalator Vibration Analytical Model during Earthquake
Koji NARIYA, Yudai TANAKA, Satoshi FUJITA, and Osamu TAKAHASHI
108
Dynamic Analysis for Vertical Movement of Elevator Governor Tension Sheave
Kotaro Fukui, Seiji Watanabe, Masaki Kato, Takeshi Niikawa
113
Estimation of main cable tension of the suspension bridge
Nguyen Huu Hung
119
Transfer-matrix-based approach for an eigenvalue problem of a drum-like rectangular cavity
Hiroyuki Iwamoto, Nobuo Tanaka
126
Transverse Motion of the Plate Spring that Automatically Follows the Excitation Frequency
Takuya Kishida, Kazumasa Ohama, Takumi Inoue, Ren Kadowaki, Kazuhisa Ohmura
131
FEM Analysis Considering Air Viscosity in Narrow Rectangular-Closs Section Pathway
Manabu Sasajima, Takao Yamaguchi, Mitsuharu Watanabe, Yoshio Koike
137
Sloshing Phenomenon Analysis by Using Concentrated Mass Model
Tatsuhiro Yoshitake, Satoshi Ishikawa, Takahiro Kondou, Kenichiro Matsuzaki
142
Study on Reliability Enhancement of Seismic Risk Assessment of NPP as Risk Management Fundamentals
(Evaluation of Seismic Response for Quantifying Epistemic Uncertainty on Fragility Assessment
of Equipment and Piping)
Osamu FURUYA, Sho ASAOKA, Ken MURAMATSU, Shigeru FUJIMOTO, Hitoshi MUTA
149
A Novel Analytical Method to Assess Transient Coupled Vibration of a Tall Building Against Downburst
Windstorms
Thai-Hoa Le, Luca Caracoglia
154
Exploring the Simulation of the Stochastic Response of a Tall Building in a Tornado-like Wind
Thai-Hoa Le, Luca Caracoglia
162
Application of Wavelet Transform to Damage Detection in Plates using Response-only Measurements
Muyideen Abdulkareem, Norhisham Bakhary, Mohammadreza Vafaei
170
Study on Seismic Enhancement Method of Hanging Type Mechanical Structure in Industrial Facilities
Osamu FURUYA, Kazuhiro YOSHIDA, Keiji OGATA and Nobuhiro NIIYAMA
177
Study, design and fabrication of “micro-electrical-generator” based on the principle of flutter phenomenon
NGUYEN Van Sy, VU Dinh Quy, DINH Tan Hung
183
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Finite element vibration analysis of viscoelastic composite structures
Zhicheng Huang, Zhaoye Qin and Fulei Chu
Determination of Dynamic Impact Factor for Continuous bridge and Cable-stayed bridge due to vehicle
braking force with experimental investigation
Toan Xuan NGUYEN, Duc Van TRAN
191
196
Response Analysis of Multiple Supported Elastic-Plastic Piping Systems for Estimating Its Maximum Response 204
Tomoyuki Matsuda, Nanako Miura, Akira Sone, Thuan Nguyen Xuan
Buckling Analysis of Laminated Shallow Shells under General Form Pressure and Boundary Condition
Tatsuya Tampo, Shinya Honda, Yoshihiro Narita
212
Study of Rolled Multi-Layer Cylindrical Shell in Frequency Domain
Can Nerse, Semyung Wang
218
Reduction of wave propagation from a curved beam to straight beams
Yuichi MATSUMURA, Kohei FURUYA, Tuyen NGUYEN BA, Hirotaka SHIOZAKI
222
Broadband Piezoelectric Energy Harvester Using a Mass Attached Near the Fixed-end
Sin Woo JEONG, Hong Hee YOO
228
Application of gas-spring damper to furniture fixture devices, a suggestion to prevent human damages
in huge earthquakes
Yukiko ISHIHARA, Satoshi FUJITA, Keisuke MINAGAWA
Structural Optimization of SEA Subsystems using Finite Element Model
Katsuhiko KURODA
232
237
Dynamic response of beam on a new foundation model subjected to a moving oscillator by finite
element method
PHAM Dinh Trung, HOANG Phuong Hoa and NGUYEN Trong Phuoc
244
Nonlinear dynamic analysis of imperfect eccentrically stiffened S-FGM thick circular cylindrical shells
on elastic foundations and subjected to mechanical loads
Nguyen Dinh Duc, Tran Quoc Quan
251
Vehicle-Cable stayed bridge Dynamic Interaction considering the vehicle braking effects using the Finite
Element Method
Toan Xuan Nguyen, Duc Van Tran
260
Nonlinear Vibration of eccentrically Stiffened Functionally Graded Toroidal Shell Segments Surrounded
by an Elastic Medium
Dao Huy Bich, Dinh Gia Ninh, Bui Huy Kien
268
Application the frequency response function to evaluate the tuned liquid damper system at the tower of
Baichay cable stayed Bridge in Viet Nam
Nguyen Duc Thi Thu Dinh, Nguyen Viet Trung and Nguyen Huu Hung
278
Axisymmetric Free vibration of Layered Conical Shells using Chebyshev Polynomial with
Collocation Method
K.K.Viswanathan, Z.A. Aziz, J.H. Lee, M.D. Nurul Izyan
286
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Section B. Vibration of Discrete Systems and Machine Dynamics
Development and Investigation of an Energy-Regenerative MR Damper
Satoru Akao, Tomoki Sakurai, Shin Morishita
Analytical Research on Dynamic Characteristics of Rolling Agricultural Tire
(Investigation of Lug Excitation Force Characteristics)
Katsuhide Fujita, Takashi Saito, Mitsugu Kaneko
295
300
Evaluation of dynamic characteristics of the rubber element with and without constraint
Shozo Kawamura, Ryosuke Isoda, Masami Matsubara
307
Proposition of a judgment method of proper paths in the transfer path analysis
Shozo Kawamura, Kota Itadani, Masami Matsubara
312
Hunting Behavior of the High Speed Railway Vehicle on a Curved Track
Yuto Yoshida, Yuki Kunimatsu, Shoichiro Takehara, Yoshiaki Terumichi
318
Vibration suppression of the large eccentric rotor by using externally pressurized gas journal bearings
with asymmetrically arranged gas supply holes
Tomohiko Ise, Takaaki Itoga, Kazuya Imanishi, Toshihiko Asami
324
Development of an Assistance System for a Two Wheeled Vehicle Using a Vibrator
Thai Quoc PHAM, Chihiro NAKAGAWA, Atsuhiko SHINTANI, and Tomohiro ITO
329
On the computation of the vibration of foil-air bearing – rotor systems
Minh-Hai PHAM, Xuan-Ha NGUYEN and Bao-Lam DANG
336
Rocking Vibration of Rigid Block under Simulated Seismic Wave
ManYong Jeong, Keita Aoshima
342
Influence on Rocking Vibration Characteristics by Minute Change of System Parameters
ManYong JEONG, Yuto Suzuki
352
Visualization of Strain Distribution in Gear Teeth under Operation by Photo-Elasticity Technique
Daisuke Yamazaki,Yusuke Hasebe,Toshihiko Shiraishi,Shin Morishita
361
Dynamics and Control of Clutchless AMTs
Paul D WALKER, Yuhong Fang, Holger Roser, Nong Zhang
368
On an approximate technique for Fokker-Planck-Kolmogorov equation in the theory of random vibration
D.N. Hao, N.D. Anh, N.C. Thang
374
Effect of radial contact area of brake pad on in-plane squeal of automotive disk brake
Yutaka Nakano, Hiroki Takahara, Noriyuki Shirasuna
380
Pedestal design for resonance separation
Hyeon-Tak Yu, Jong-Myeong Lee, Gyu-Jin Park , Hack-Eun Kim and Byeong-Keun Choi
386
Research on natural vibration characteristics for change of a sliding part in a reciprocating compressor
Yoshifumi MORI, Takenori NAKAMURA, Katsuhide FUJITA and Takashi SAITO
391
Analysis of coupling vibration between tire flexible ring and rigid wheel model
Masami MATSUBARA, Makoto HORIUCHI, Shozo KAWAMURA, Fumihiko KOSAKA
395
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Small and simple isolation table using coil springs
Taichi Matsuoka, Tomonori Niwa, Tenma Takayanagi, Kenichiro Ohmata
400
Study on wear behavior analysis of tire using the distributed lumped mass-spring model
Yu Koketsu, Shoichiro Takehara, Yoshiaki Terumichi, Zenichiro Shida, Toshiyuki Ikeda
406
Geometric illustration of several stochastic equivalent linearization criteria
Anh NGUYEN DONG, Linh NGUYEN NGOC
413
Basic Research on a Novel Zero-Emission Public Transportation System (Investigation of Consumption
Energy using a Simple Electric Bus Simulator for an Electric Bus System with Rapid Charging at Every
Bus Stop using Renewable Energy)
Takeshi Kawashima
419
Dynamic model of rocking vibration for free standing spent fuel rack
Akihiro TAKAI and Shigehiko KANEKO
427
An analytic study on the Structural Safety of Two-spindle System
Min Jae Shin, Dong Il Kim, Jae Deok Hwang, Chae Sil Kim, and Hun Oh Choi
435
Inverse Sub-structuring Theory for Coupled Mechanical System with Incomplete Measured Data based
on the Dummy Masses
Qi-li Wang, Jun Wang, Li-xin Lu, An-jun Chen, Huan-xin Jiang
440
Dynamic modeling and investigation on the electromagnetic vibration of an eccentric rotor with
bearing forces
Xueping Xu, Qinkai Han, and Fulei Chu
448
Rub-impact Analysis of a Disk-drum Rotor System
Lumiao Chen, Zhaoye Qin, and Fulei Chu
456
Simulation and Analyses of Dynamic Gust Responses of a Flexible Aircraft Wing under Continuous Random
Atmospheric Turbulence
Anh Tuan Nguyen, Jae-Hung Han
461
Analytical model building and vibration reduction of drum-type washing machines at high rotational speeds
Nobutaka TSUJIUCHI, Akihito ITO, Mami YOSHIDOMI, Hiroki SATO
468
Fundamental study of subharmonic vibration in automatic transmission
Akihiro NANBA, Takashi NAKAE, Takahiro RYU, Kenichiro MATSUZAKI, Sofian ROSBI,
Yoshihiro TAKIKAWA, Yoichi OOI, Atsuo SUEOKA
475
A fractal friction contact model and its application in forced response analysis of a shrouded blade
Hengbin Qiu, Zili Xu, Chunmei Zhang
483
A Study for LNG Pump Shaft Balancing by the Rig
Yong Ho Jang, Hyo Jung Kim, Jong Myeong Lee, Sun Hwi Park, Hack Eun Kim, and Byeong Keun Choi
491
Research and Development of Laminated Bearing for Base-Isolation System using Urethane Elastomer
Kenta Ishihana, Osamu Furuya, Kengo Goda, Shohei Omata
494
Effects of the Non-linear Restoring Force Characteristics of the Rubber Bearings on Seismic Isolated Building
Yuki HASE, Satoshi FUJITA, Keisuke MINAGAWA
500
Analysis of Pulse Wave in Blood Vessel by Concentrated Mass Model
Satoshi Ishikawa, Takahiro Kondou, Kenichiro Matsuzaki
506
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Dynamic Stability Derivative Measurement of the MAV Model Using Magnetic Suspension Balance System
Chang-Beom Kwon, Dong-Kyu Lee, Jae-San Yoon and Jae-Hung Han
Multi-physical analysis of an eddy current damper (ECD) for a reaction force compensation (RFC)
mechanism of a linear motor motion stage
Kang Jo Hwang, Canh Nguyen, Jae Seong Jeong, Hyeong Joon Ahn
Detection of blade rub in rotor system
W. K. Ngui, M. Salman Leong, M. H. Lim, and K. H. Hui
A Hybrid Method of Support Vector Machine and Dempster-Shafer Theory for Automated Bearing
Fault Diagnosis
K.H.HUI, L.M.HEE, M. Salman LEONG, M.K. ZAKARIA, and W.K. NGUI
512
516
521
525
A Method for Solving the Motion Equations of Constrained Systems
Sanh Do, Phong Dinh Van, Khoa Do Dang, Tran Duc
532
Reliability Analysis of Motorized Spindle based on ANSYS and BP Neural Networks
Zhou Yang, Panxue Liu, Hao Wang, Yimin Zhang and Xianzhen Huang
538
Torsional rigidity analysis of cycloid reducers considering tolerances
TheLinh TRAN, AnhDuc PHAM, ChungIl CHO and HyeongJoon AHN
546
A study on applying a Dynamic model to determine the Body roll center of Heavy Trucks
Khanh Duong Ngoc, Huong Vo Van and Hung Ta Tuan
552
Structural and Vibration Analysis Considering the Flow Velocity of the Heat Exchanger
Yong-Seok Kim, Byung-hyun Ahn, Jung-Min Ha, Seok-Man Son and Byeong-Keun Choi
555
The Forced Response of a Time-Delayed Nonlinear System under Two Families of Additive Resonances
J.C. Ji, Terry Brown
560
Experimental Investigation of a Roll-plane Hydraulically Interconnected Suspension and Anti-roll Bars
in Warp Mode
Nong ZHANG, Sangzhi ZHU and Jack Liang
566
Dynamic Theory and Experiments of a New Near-Resonant Vibrating Screen with Inertial Exciter
Wen Bangchun, Liu Shuying, Wang Zongyan, Zhang Xueliang
571
The Receptance Incremental Harmonic Balance Method for Analyzing Rubbing Rotor System
YAO Hongliang, LIU Ziliang and WEN Bangchun
576
The Method of High Order Fatigue Test of Thin Plate Composite Structure with Hard Coating
Hui Li, He Li, Zhaohui Ren, Bangchun Wen
582
Dynamic Analysis of the Feed Drive System for a Lathe
ZHAO Chunyu, CHEN Ye, FAN Chao and WEN Bangchun
588
Analysis on the Material Movement of Solid Wastes Processing Screen
Jing JIANG, Yan WU, Shuying LIU and Bangchun WEN
593
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Section C. Control and Optimization of Dynamic Systems
Design of resonance frequency of smart Helmholtz resonator using neural network
Wakae Kozukue, Hideyuki Miyaji
601
Efficiency Examination of Automatic Digging for Excavators on Several Conditions
Tatsuya Yoshida, Nobutaka Tsujiuchi, Akihito Ito, Fumiyasu Kuratani, Hiroaki Andou
606
Optimal Design of Dynamic Absorber for Subharmonic Nonlinear Vibration in Automatic Transmission
Powertrain
Takashi Nakae, Takahiro Ryu, Kenichiro Matsuzaki, Sofian Rosbi, Atsuo Sueoka, Yoshihiro Takikawa,
Yoichi Ooi
614
An improved pendulum dynamic vibration absorber with radial vibration mode excited by centrifugal force
La Duc Viet, Nguyen Ba Nghi
623
Admittance Control System without Force Sensor for Master-slave Rehabilitation
Masashi Yamashita
628
Advanced sliding mode control of floating container cranes
Pham Van Trieu, Hoang Manh Cuong, Le Anh Tuan
633
Parameter Optimization of Tuned Mass Damper Systems to Human Body Vibration Control
for Standing and Sitting Postures
Nguyen Anh Tuan, Nguyen Van Khang and Trieu Quoc Loc
643
Increase of critical flutter wind speed of long-span bridges using passive separate control wings
Nguyen Van Khang, Tran Ngoc An
649
Robust design of a composite antenna structure by using multi-objective Taguchi method
Soichiro Tanaka, Shinya Honda, Yoshihiro Narita
655
Operating mechanism and optimization of dynamic absorber for a negative damping system
Tomoyuki TANIGUCHI and Takahiro KONDOU
662
Trajectory Planning Method for Anti-Sway Control of a Rotary Crane
Akira Abe, Keisuke Okabe
668
Vibration Control of Overhead Traveling Crane by Elimination Method of Natural Frequency Components
(Complete Prevention of Residual Vibration of Cargo)
Toru MIZOTA, Takahiro KONDOU, Kenichiro MATSUZAKI, Nobuyuki SOWA, Hiroki MORI
673
Vibration Mitigation of Thermal Power Plants due to Earthquake by Installing Viscous-Friction
Hybrid Dampers
Ryo Kato, Satoshi Fujita, Keisuke Minagawa, Go Tanaka
679
Fundamental Study on Health Monitoring System for Pipe using Acceleration of its Surface
Kimihiko Inami, Satoshi Fujita, Keisuke Minagawa,Mutsuhito Sudo
686
Suppression of Low Frequency Vibration of a Vibroimpact System by a Dynamic Absorber
Hiroki Mori, Takuo Nagamine, Takanori Kobayashi, Yuichi Sato
690
Active wave control of a coupled rectangular cavity
Motoya Watanabe, Hiroyuki Iwamoto, Nobuo Tanaka
694
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Semi-active control of RFC (reaction force compensation) mechanism for a linear motor motion stage
Duc-Canh NGUYEN, Kang-Jo HWANG, Hyeong-Joon AHN
Design method of PID controllers for active mass damper systems
incorporating neural oscillators
Junichi HONGU, Daisuke IBA, Takayuki SASAKI, Morimasa NAKAMURA, and Ichiro MORIWAKI
702
708
Evaluation of the current Health Monitoring Systems for Cable-stayed Bridge in Vietnam
DAO Duy Lam, NGUYEN Viet Trung
714
Adaptive Vibration Control Based on Pole Tuning of Model-based Controller
Keiichiro FURUYA, Shinichi ISHIZUKA, Itsuro KAJIWARA
718
Development of Wire Driven Active Vibration Suppression for Gantry Crane with Mechanical Control
Yasuo AOKI, Takashi AOKI, and Yasutaka TAGAWA
725
Bilateral Tele-robot of Multiple Cooperative Robots control based on PD method and virtual damping
with time delay
Thuan Nguyen, Tomoyuki MATSUDA, Hung Chi Nguyen, Nam Duc Do, Akira SONE, Nanako MIURA
730
A Fuzzy Logic System Built based on Fuzzy Data Clustering and Differential Evolution for Fault Diagnosis
Sy Dzung Nguyen, Quang Thinh Tran, Kieu Nhi Ngo, Tae Il Seo
738
An Adaptive Dynamic Inversion Controller for Active Railway Suspension Systems
Sy Dzung Nguyen, Kieu Nhi Ngo, Nang Toan Truong, Vien Quoc Nguyen, Tae Il Seo
746
Acceleration control of an electric skateboard considering postural sway
Motomichi Sonobe, Hirotaka Yamaguchi, and Junichi Hino
754
Vibration analysis and stacking sequence optimization of laminated rectangular plate with blended layers
Fumiya NISHIOKA , Shinya HONDA , Yoshihiro NARITA
760
Control of cable vibration using friction damper with consideration of bending stiffness
Duy-Thao NGUYEN, Xuan-Toan NGUYEN
767
Controller Design Strategy to Improve Broad Band Tracking Performance for Shaking Tables
Mineki Okamoto, Yasutaka Tagawa
774
Control Simulation of an Electrically-Controlled Variable Valve Timing (ECVVT) System with
Cycloid Reducer
ChungIl Cho, JaeSeong Jeong and HyeongJoon Ahn
780
Motion Investigation of Planar Manipulators with a Flexible Arm
Sanh Do, Phong Phan Dang, Khoa Do Dang, Binh Vu Duc
784
Influence of models on computed torque of delta spatial parallel robot
Nguyen Quang Hoang, Nguyen Van Khang, Nguyen Dinh Dung
791
Input Shaping and PD Controller for Double-Pendulum Overhead Cranes
Nguyen Quang Hoang, Nguyen Van Quyen and Dinh Van Phong
799
Semi-active Suspension Control of a Semi-trailer Truck using Magnetorheological Fluid Damper
Sardar Muhammad IMRAN and Zhichao HOU
806
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Section D. Vibration and Noise
Global active noise control using a parametric beam focusing source
Nobuo Tanaka and Motoki Tanaka
817
Sensing of Nanotoxic Material using Resonance Frequency
Kuehwan Jang, Junseok You, Chanho Park, Jinsung Park, Sungsoo Na
823
Standardization of scaled HRIRs based on multiway array analysis
Daehyuk Son, Youngjin Park
826
Experimental Study on Vibration and Noise of Wet Friction Clutches
Junya Kamei, Toshihiko Shiraishi
831
Prediction of dynamic behavior of workpieces in ultrasonic plastic welding
Takao Hirai, Fumiyasu Kuratani, Tatsuya Yoshida, Saiji Washio
837
Broadband Energy Focalization Using a Tailored Power-law-profiled Indentation with Lens-like Function
Wei Huang, Hongli Ji, Li Cheng, Jinhao Qiu
844
Experimental study on vibration and noise phenomenon generated from small fan motors
Koki Shiohata, Masaki Ogushi
850
Study on Noise Reduction Method of Acoustic Emission Signal for Rotorcraft Gearboxes Condition
Monitoring and Diagnosis
ByungHyun Ahn, HyoJung Kim, Sun Hwi Park, YongSeok Kim, OeCheul John Kim and Byeong Keun Choi
855
Development of Simulator of Allophone of Motors for Automobiles-Extended Transfer Function
Synthesis Method for Analysis Object Including Enclosed Acoustic Field and Motor
860
Koji Kobayashi, Seiji Nishida, Yoshifumi Morita, Makoto Iwasaki, Ryo Kano, Yasuhiko Mukai, Hideki Kabune,
Norihisa Ito
Active control of sound transmission through a panel with feedforward and feedback control
Akira SANADA, Nobuo TANAKA
866
New Evaluation Technique of Seal Strength of Heat Sealing with Ultrasonic Pulse
Ren Kadowaki, Takumi Inoue, Tatsuya Oda, Takahiro Nakano
871
Model-based active noise control by a concentrated mass model
Shotaro Hisano, Satoshi Ishikawa, Shinya Kijimoto, Yosuke Koba
878
Vibration of glass panel fixed by adhesive tape of mobile phone
Yoshihiko KAITO, Shinya HONDA, and Yoshihiro NARITA
886
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Preface
The Asian Pacific Vibration Conference (APVC) is an international conference held once every two
years with the intention of encouraging scientific and technical cooperation among Asia Pacific
countries. The conference aims to bring researchers, engineers and students from but not limited to areas
around the Asia Pacific countries in a collegial and stimulating environment to present the most recent
developments and new information on any aspect of mechanical vibration and sound.
The 16th APVC (APVC 2015) was held in November 24-26, 2015 at Hanoi University of Science and
Technology, Vietnam. The previous fifteen series conferences were held in Japan (1985), Korea
(1987), China (1989), Australia (1991), Japan (1993), Malaysia (1995), Korea (1997), Singapore
(1999), China (2001), Australia (2013), Malaysia (2005), Japan (2007), New Zealand (2009), Hong
Kong (2011), Korea (2013).
The program of APVC 2015 covered a broad spectrum of theoretical, computational, and experimental
topics in vibration, control, and sound. The invitation to this meeting resulted in a participation by
about 200 scientists from 11 different countries. During the conference about 150 lectures are
presented. Some of the research areas were

Vibration of continuous systems and structure dynamics

Vibration of discrete systems and machine dynamics

Control and Optimization of dynamic systems

Vibration and Noise
The organization of this conference would not be possible without the support and contributions from
many individuals and organizations. We sincerely appreciate the support from Hanoi University of
Science and Technology (HUST) and Vietnamese Association of Mechanics (VAM).
We would like to thank the support of Department of Applied Mechanics of HUST and the members
of the Local Organizing Committee for their generous assistance during the meeting and the
preparation of this proceedings.
November 2015
Yoshihiro Narita, Hokkaido, Japan
Nguyen Van Khang, Hanoi, Viet Nam
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16th Asia Pacific Vibration Conference
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APVC2015
Advanced sliding mode control of floating container cranes
Pham Van Trieu*, Hoang Manh Cuong*, and Le Anh Tuan*,#
*
Institute of Research and Development, Vietnam Maritime University, Hai Phong, Viet Nam
#
Corresponding Author / E-mail: tuanla.ck@vimaru.edu.vn
wave-induced motions of a ship by controlling the
boom-luff angle. Rahman et al. [7] reduced payload
pendulations due to near-resonance excitations using the
reeling and unreeling of handling cable. Masoud et al. [8]
suppressed payload vibrations by controlling both slew and
luff angles of the boom. Chin et al. [9&10] provided a
model of boom crane as an elastic spherical pendulum. A
nonlinear model was solved by the method of multiple
scales to find the approximated solutions. Wen et al. [11]
constructed a dynamic model of a boom crane on a ship
with Maryland Rigging, investigated the controllability and
observability of linearized model, and designed an optimal
controller based on linear quadratic regulator to reduce the
payload pendulation. Ellermann et al. [12&13] studied
nonlinear dynamics of boom crane vessels. Maczynski and
Wojciech [18] proposed an auxiliary mechanical system to
stabilize the position of load in ship-mounted boom cranes.
Kimiaghalam et al. [19] constructed a feed-forward
controller for a shipboard boom crane using
gain-scheduling technique. Fang and Wang [20] proposed a
nonlinear controller for ship-based boom crane using
Lyapunov technique. Spathopoulos et al. [21] designed an
active control system for reducing payload pendulation of
an offshore crane based on linear quadratic Gaussian and
generalized predictive control. Schaub [22] discussed two
active ship motion compensation strategies to reduce cargo
swing for offshore boom crane. Newly, Cha et al. [23]
analyzed the dynamic behavior of a floating heavy crane in
which the mathematical model was described by 12
nonlinear equations of motion.
Several recent articles have focused on control of
container crane mounted on rigid foundation [24-27]. With
a simplified model of container crane, a delayed feedback
law was investigated in paper [24]. Masoud et al. [25]
developed a new model for container crane in which
container was considered a rigid body handled on four rigid
cables. Then, the time-delay controller was designed for a
simplified version of this model to reduce container sway
and track the trolley. Linearizing the model of article [25],
Nayfeh et al. [26] created a time-delay feedback controller,
determined the normal form of the Hopf bifurcation using
technique of multi-scales, and investigated the robustness
of proposed controller.
Abstract
This article constructs two robust controllers using sliding mode
control (SMC) techniques. The ship-crane system is operated in
the complicated condition in which the disturbances due to
viscoelasticity of seawater and the flexibility of handling cable are
fully taken into account. With two actuators composed of
trolley-moving force and container-hoisting torque, the controllers
concurrently stabilize six states consisting of trolley displacement,
container lifting motion, container swing, axial container
oscillation, ship roll and heave. The quality of control algorithms
is investigated thru simulation. The results show that the
responses of crane are asymptotically stabilized and ship
vibrations are significantly reduced.
Keywords: cranes; sliding mode control; under-actuated system;
system modeling;
1. Introduction
Container cranes play an important role in cargo
transportation. Recently, the rapid development of world
logistics and transportation industry trends to construct a
lot of large container ships. Many large harbors in the
world are the river-ports with narrow and shallow channels.
The big container ships cannot reach into such the harbors.
In this case, the cargo transferring process must be done in
the area of sea buoy outside the domestic port. A container
crane mounted on a ship (as seen in Fig. 1) is applied to lift
and transfer containers from the large ship to small ships.
Subsequently, small ships will carry containers to the
terminal. To increase the productivity, modern container
cranes are required in speedy operation. Without good
control strategies, the fast crane motion usually leads to the
large cargo swings and non-precise movements. Then,
crane and ship can be destabilized.
Until now, numerous theoretical researches as well as
application papers studying on dynamics and control of
cranes have been published [1-27]. However, the number of
papers concerning on ship-mounted cranes is quite small,
compared with that of onshore crane studies. Concentrating
on boom crane mounted on vessel, a lot of articles have
been reported. Using delay position feedback method,
Henry et al. [6] reduced the cargo pendulations caused by
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HUST, Hanoi, Vietnam
APVC2015
Study on dynamics and control of container crane
attached on ship has not attracted numerous researchers.
Based on a simplified linear model of offshore crane,
Messineo et al. [27] presented an adaptive controller to
reduce the hydrodynamic slamming load and track the
payload according to a given velocity.
Encouraged by recent works [25&26] of Nayfeh’s
group, we focus on dynamics and robust controls of
ship-mounted container crane which has the improving
points as follows:
(i) Dissimilar to the articles [25&26] where container
crane is mounted on rigid foundation, we claim that the
container crane-ship system is suspended on damper-spring
foundation characterized for viscoelasticity of seawater.
Therefore, the proposed controllers will be designed for the
case that disturbance due to elastic-damping property of
ocean water is fully included. Furthermore, we consider a
ship as a rigid body described by mass and moment of
inertia. Therefore, impact of ship motions on container
crane is clearly the dynamic excitations.
(ii) While preceding articles [1-27] assumed that cable
was a hard (inelastic) string, this study considers
container-handling cable as the elastic damping rope that is
close to realistic crane system in practice. Therefore, the
action of disturbance due to elasticity of handling cable is
included in robust controllers design, as we will see later.
Normally, the cargo transferring process of container
crane consists of three separated phases: lifting the payload,
moving the trolley, and lowering the payload. To increase
the efficiency, these phases can simultaneously be
combined. The mathematical model and robust controllers
are constructed in the complicated operating case in which
hoisting the container and pulling the trolley are
simultaneously started. The system behavior is described
by six fully nonlinear equations of motion. Correspondingly,
six outputs composed of trolley movement, rotation of hoist,
container’s oscillation along the cable, container swing, roll
and heave motions of ship are considered. The effects of
ship roll and heave, the viscous-elasticity of ocean water,
the elasticity of hoisting rope are fully taken into account in
modeling the ship crane-system and designing the
controllers. Since only two inputs composed of trolley
pulling force and torque of hoist are used to drive six
outputs, the mathematical model is separated into actuated
dynamics and un-actuated dynamics. Two robust nonlinear
controllers are designed using conventional and
back-stepping SMC approaches. The simulation is carried
out to investigate the controller quantity. The effects of
disturbances due to viscoelasticity of seawater and
flexibility of wire rope are fully considered in two
simulation cases.
Fig. 1. A container crane mounted on a ship
Fig. 2: Physical modeling of a floating container crane
2. System dynamics
A container crane attached on a ship (Fig. 1) is
modeled as a multi-body system shown in Fig. 2. Ship is
considered as a rigid body having its center mass mb and its
moment of inertia Jb. Ship is suspended on stiffness and
damping components k1, k2, b1, b2 characterized for
elasticity and viscous damping of seawater. Container
handled on flexible cable is viewed as a point mass mc. The
flexibility of cable is characterized by spring k3 and damper
b3. Trolley is pushed by force ut to move along the primary
beam of crane. Hoisting mechanism is fixed on trolley base
and the container is lifted or lowered by rotating a drum
having radius rm and moment of inertia Jm. The dynamical
behavior of system is analyzed in the complicated
operating case in which hoisting the container and moving
the trolley are simultaneously implemented. The dynamic
system set in reference Cartesian frame Oxy composes of
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HUST, Hanoi, Vietnam
APVC2015
two rigid bodies, namely ship’s body (mb, Jb) and hoisting
drum Jm, and two particles, namely trolley mass mt and
container mass mc. The mechanical system has six degrees
of freedom associated with six generalized coordinates:
trolley motion along the primary beam of crane
m35  mc (l0  s  q4  rm q3  rm q2 )sin q3 ,
m36  mc a2 (l0  s  q4  rmq3  rm q2 )cos(q6  q3 )
 mc (l0  s  q4  rm q3  rm q2 )(q1  a1 )sin(q6  q3 )
q1  xt , rotation of hoisting drum q2   m , container swing
m41  mc sin(q6  q3 ) , m42  mc rm , m44  mc ,
q3   ,
m45  mc cos q3 , m51  (mc  mt )sin q6 ,
container
oscillation
along
the
cable
q4  s, vertical oscillation of ship q5  y, and ship swing
m46  mc (q1  a1 ) cos(q6  q3 )  mc a2 sin(q6  q3 )
q6  b . Two actuators compose of trolley pulling force
m52  mc rm cos q3
equations, we constituted the fully nonlinear equation of
motion in paper [28] as follows
where,
M  q    mij 
C  q, q   cij 
G  q    g j 
U  u1  ut
T
is
m53  mc (l0  s  q4  rm q2  rm q3 ) sin q3 ,
m56  (mt  mc )a1  (mt  mc )q1  cos q6
(1)
symmetric
mass
matrix,
damping
matrix,
 (mt  mc )a2 sin q6
,
m61  (mc  mt )a2 ,
denotes
centrifugal
m62   J m  mc rm (q1  a1 ) cos(q6  q3 )
( i, j  1  6 ) indicates a gravitational vector,
u2  M m
,
m54   mc cos q3 , m55  mt  mb  mc ,
ut and torque M m of lifting drum. Based on Lagrange’s
  C  q, q  q  G  q   U
M q q
,
 mc a2 rm sin(q6  q3 )
m63  mc a2 (l0  s  q4  rm q2  rm q3 ) cos(q6  q3 )
0 0 0 0 is a vector of inputs,
T
 l0  s  q4 
 mc 
 (q1  a1 ) sin(q6  q3 )
  rm q3  rm q2 
and q   xt m  s y b    q1 q2 q3 q4 q5 q6  is
T
T
a vector of generalized coordinates.
m65  (mt  mc )(a1  q1 ) cos q6  (mt  mC )a2 sin q6 ,
m11  mc  mt , m12  mc rm sin(q6  q3 ) ,
m66  J b  J m  (mt  mc )(q12  a12  a2 2  2a1q1 ) ,
m13   mc (l0  s  q4  rm q2  rm q3 ) cos(q6  q3 ) ,
m23  m32  m34  m43  0.
m14  mc sin(q6  q3 ) , m15  (mt  mc )sin q6 ,
The elements of damping matrix is of the form
m16  (mt  mc )a2 , m21  mc rm sin(q6  q3 ) ,
c11  bt , c12  2mc rm q3 cos(q6  q3 ) ,
m22  J m  mc rm2 , m24  mc rm , m25  mc rm cos q3 ,
c13  mc (rm q3  2q4 ) cos(q6  q3 )
 mc rm (q1  a1 ) cos(q6  q3 )
,
m64  mc (q1  a1 ) cos(q6  q3 )  mc a2 sin(q6  q3 ) ,
The components of mass matrix has the following form
m26   J m  mc rm a2 sin(q6  q3 )
,
 mc (l0  s  q4  rm q3  rm q2 )q3 sin(q6  q3 )
,
,
c16  (mt  mc )(a1  q1 )q6 , c21  2mc rq6 cos(q6  q3 ) ,
m31  mc (l0  s  q4  rm q3  rm q2 ) cos(q6  q3 ) ,
c22  bm , c23  mc rm (l0  s  rm q4  rm q2 )q3 ,
m33  mc (l0  s ) 2  mc q4 2  mc rm2 (q3  q2 ) 2
c26  mc rm (q1  a1 )q6 sin(q6  q3 )  mc rm a2 q6 cos(q6  q3 )
 2mc (l0  s )q4  2mc rm (q2  q3 )(l0  s ) ,
 2mc rm  q2 q4  q3 q4 
,
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APVC2015
3. Controllers design
c31  2mc (l0  s  q4  rm q3  rm q2 )q6 sin(q6  q3 ) ,
In this section, two robust controllers are constructed
using conventional and advanced sliding mode techniques.
The controllers are applied for stabilizing offshore
container crane in its complicated operation in which lifting
the container and moving the trolley are simultaneously
combined. More precisely, the controllers simultaneously
conduct seven duties: tracking the trolley to destination,
hoisting the container to desired cable length, suppressing
the axial oscillation of container caused by cable elasticity,
maintaining the container swing small during
transient-state and completely eliminating this swing at
steady-state, reducing the heave and roll motions of ship as
small as possible.
3.1 Decoupling
A container crane mounted on a ship has six degrees of
freedom associated with six output components,
c32  2m c rm (l0  s  q4  rm q3  rm q2 )q3 ,
c33  mc (l0  s  q4  rm q2  rm q3 )(2q4  rq3 ) ,
 l0  s  q4 
c36  mc 
 (q1  a1 ) cos(q6  q3 )q6
,
  rm q3  rm q2 
 mc a2 (l0  s  q4  rm q2  rm q3 ) sin(q6  q3 )q6
c41  2mc q6 cos(q6  q3 ) , c44  b3 ,
c43  mc (l0  s  q4  rm q2  rm q3 )q3 ,
c46  mc (q1 +a1 ) sin(q6  q3 )q6  mc a2 cos(q6  q3 )q6 ,
c51  2(mt  mc ) cos q6 q6 , c55  b1  b2 ,
q   q1
c53  mc (l0  s  q4  rm q2  rm q3 ) cos q3 q3
,
 mc (rm q3  2rq2  2q4 ) sin q3
U  u1 u2
q a   q1
c61  2(mt  mc )(q1  a1 )q6 ,
q6  . As an under-actuated
T
q5
0 0 0 0 in which only actuated states
T
q2 
T
are directly tracked by control forces
T
qu   q3
q4
q5
The
q6 
T
un-actuated
states
are not connected directly to
actuators. Corresponding to actuated and un-actuated states,
the mathematical model (1) can be decomposed into two
sub-systems as
c65  b2 a4  b1a3 , c66  b2 a4 2  b1a3 2 ,
c14  c15  c24  c25  c34  c35
 c42  c45  c52  c54  c62  c64  0.
and the coefficients of gravity vector is determined by
 a  M12 (q )q
u  C11 (q, q )q a
M11 (q )q
C12 (q, q )q u  G1 (q)  U1 (q, q )
(2)
a  M 22 (q)q
u  C21 (q, q )q a
M 21 (q)q
C22 (q, q )q u  G 2 (q)  041
(3)
where,
g1  (mt  mc ) g sin q6 , g 2  mc grm cos q3 ,
 m m12 
m13 m14 m15 m16 
M11  q    11
 , M12  q    0 m m m 
m
m
 21

22 
24
25
26 
g3  mc g (l0  s  q4  rm q2  rm q3 )sin q3 ,
m31 0 
m33 0
m m 
 0 m
42 
44
, M22  q  
M21  q   41
m51 m52 
m53 m54



m61 m62 
m63 m64
g 4  k3 (q4  s )  mc g cos q3 ,
,
c
C11  q, q    11
 c21
g 6  (k1a3  k2 a4 )(q5  y )  (k1a32  k 2 a4 2 )q6
 (mt  mc ) g (a1  q1 ) cos q6
q4
U1  u1 u2  .
(q1  a1 )(2q4  2rm q2  rm q3 )

c63  mc 
 sin(q6  q3 )







a
(
l
s
q
r
q
r
q
)
q
4
m 3
m 2
3
 2 0
,
a2 (2q4  2rm q2  rm q3 ) 


 mc (q1  a1 )(l0  s  q4  cos(q6  q3 )
r q  r q )q

 m 3 m 2 3

 (k1  k2 )(q5  y )
q3
system, six output variables are driven by two input signals,
c56  b2 a4  b1a3  (mt  mc )a2 cos q6 q6
,
 (mt  mc )(a1  q1 ) sin q6 q6
g5  (mb  mt  mc ) g  (k1a3  k2 a4 )q6
q2
.
 (mC  mt ) ga2 sin q6
636
c12 
c
, C12  q, q    13

c22 
 c23
m35 m36 
m45 m46 
m55 m56 

m65 m66 
0 0 c16 
0 0 c26 
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APVC2015
c31 c32 
c33 0 0
c

c
0
c
0
, C22  q, q    43 44
C21  q, q    41
c51 0 
c53 0 c55



c61 0 
c63 0 c65
G1  q    g1
g 2  , G 2  q    g3
T
g4
c36 
c46 
c56 

c66 
s  e a   e a  eu
 1
0
The matrices and vectors of equation (13) is now
reduced as
reference positions q ad   q1d
states qu   q3
q4
qud   q3d  0 q4
q5
q5
where,
q6  reaching to desired values
Since
(9)
(10)
K
is
a
diagonal
positive
gain
matrix,
control input (10) makes the system trajectories remain on
the surface (7).
3.3. Stability analysis of sliding surface
Let us investigate the stability of sliding regime by
considering a positive definite function
1
V  sT s
(11)
2
The derivative of V with respect to time is defined as
M 22 (q ) is positive definite for every q  R , un-actuated
dynamics (3) can be rewritten as
(4)
Substituting equation (4) into equation (2), one obtains
the reduced form of system dynamics
V  sT s
a  C1 (q, q )q a  C2 (q, q )q u  G(q)  U1 (q, q ) (5)
M(q)q
(12)
Substituting (8) into (4) yields
where,
 2 q a  q u  T   q a  q ad  
 a   
q

 q u  K sgn  s 

1
22
M (q )  M11 (q)  M12 (q)M (q )M 21 (q)
C1 (q, q )  C11 (q, q )  M12 (q)M 221 (q )C21 (q, q )
(13)
Inserting (13) into (8) and (10) into (12), one obtains
the negative semi-definite function
C2 (q, q )  C12 (q, q )  M12 (q)M 221 (q)C22 (q, q )
G (q)  G1 (q)  M12 (q)M 221 (q)G 2 (q)
V  sT  s  sT K sgn  s  
Considering q a as system outputs, actuated dynamics

 a  M 1 (q) U1 (q, q )  C1 (q, q )q a  C2 (q, q )q u  G (q )
q
(14)
 1 s12   2 s22  K1 s1  K 2 s2  0
(5) is modified as

(8)
function of the sliding surface. The component sgn  s  of
6
a  C21 (q, q )q a 
M (q )q
u  M 221 (q )  21
q

C22 (q, q )q u  G 2 (q) 
are
0 
K  diag  K1 , K 2  , K1 , K 2  0 , sgn  s  denotes the sign
T
asymptotically.
2 
 C1  q, q  q a  C2  q, q  q u  G  q 
approaching to
T
q6 d  0
3  4
 2 q a  q u  T   q a  q ad  
U1  q, q   M  q  

 q u  K sgn  s 

q2 d  , and un-actuated
T
0
leads to the conventional SMC law
3.2 Conventional sliding mode control
Mathematically, the control schemes are designed to
q2 
0
0
s   s  K sgn  s   0
T
drive the actuated states q a   q1
1
Inserting (6) into (7) and (8) into the exponential
approaching dynamics
G 2  q   , U(q, q )   U1 (q, q ) 041 
T
and   
 a   q a  q u
s  q
M  q M12  q 
C11  q, q  C12  q, q  
M q   11
 , C q, q   

M21  q M22  q
C21  q,q  C22  q, q  
G  q   G1  q 
 2 
matrices of positive parameters.
Derivative of s with respect to time is determined by
T
T
0
where, s  R 2 ,   
g6  .
g5
(7)
which implies that V  t   V  0  for every
(6)
and
with M (q) being a positive definite matrix.
 K1 , K 2    0, 0  .
 1 ,  2    0, 0 
This means that s is limited in a
boundary. Barbalat’s lemma indicates that lim V  0 leads
t 
Defining the switching manifold as linear combination
of tracking errors e a  q a  q ad and eu  q u  q ud , we
to lim s  0 . Hence, the sliding surface is asymptotically
have
stabilized.
3.4 Back-stepping sliding mode control
t 
637
16th Asia Pacific Vibration Conference
24-26 November, 2015
HUST, Hanoi, Vietnam
APVC2015
prove that s  0 as t   . Referring from sliding
surface defined by (7), the asymptotical stability of sliding
Let us design a controller based on the combination of
back-stepping and SMC approaches. Consider a Lyapunov
lower-bounded function
1
V1  eTa e a
(15)
2
whose derivative with respect to time is described by
V1  e Ta ea
surface s and that of actuated tracking error e a lead to
zero-convergence of un-actuated tracking error eu.
4. Numerical simulation and results
(16)
The system behavior is investigated thru simulation.
The mathematical model (2)&(3) is numerically analyzed
based on MATLAB environment for three following cases:
(i) Uncontrolled case. The crane lifts the container,
and at the same time, moves the trolley to desired position.
The inputs composed of trolley driving force and torque of
hoist are determined in terms of motor performance curves.
For example, the inputs of three-phase induction AC
motors can be analytically represented as
Referring to fictitious input e a from sliding surface
equation (7), or letting fictitious input e a  s   e a  eu to
asymptotically stabilize actuated tracking error e a , then
inserting it into (15), one derives
V1  sT e a  eTa  e a  eTa eu
(17)


t 
U s  U max  U s  1  
ut (t )  
t
ts 


0

If s  0 then V1  0 or V1  t   V1  0  for every
positive definite matrix  and positive control gains .


t 
 M s   M max  M s   1  
M m t   
t
ts 


M
 s
Therefore, e a is bounded. Applying Barbalat’s lemma, we
ea  0
can conclude that
as
t   . Next step,
considering
1
V2  V1  sT s
2
as a composite Lyapunov candidate, we obtain
V2  V1  sT s = sT e a  eTa  ea  eTa eu  sT s
(23)
if t  tts
if t  tts
(24)
if t  tts
where, U s  k f  mc  mt  g and M s  mc rm g are static
(18)
force and torque at steady-state,
U max , M max
are
maximum starting force and torque at transient-state
(19)
determined from motor’s catalogs, tts is time duration of
Inserting (6) into (8) and (10) into (19) yields
V2 = sT e a  eTa  e a  eTa eu

U1  q, q   C1  q, q  q a 
 M 1  q  

s 
C2  q, q  q u  G  q  


  q a  q u

if t  tts
transient-state, k f is coefficient of kinetic friction.
as back-stepping SMC input, we obtain the derivative of
(ii) Conventional SMC and back-stepping SMC. The
dynamics (2)&(3) of crane-ship system is respectively
driven by conventional SMC input (10) and back-stepping
SMC input (21). The system parameters and gains of
controllers used for simulation are depicted in Table 1.
Controller parameters are chosen based on trial and error
method.
The controllers (10) and (21) will move the trolley
suspending container to 3 m – desired position,
concurrently lift the container from initial cable length l0 =
V2 which is described by
15 m to ld  l0  rm md  s  12 m – desired cable length in
T
(20)
Choosing
U1  q, q   C1  q, q   M  q   q a
 C2  q, q   M  q   q u
(21)
 M  q  q a  q ad   G  q   M  q   sgn  s 
V2  V1  sT s = V1  sT  sgn  s 
= V   s   s  0
1
1
1
2
terms of the number of desired revolution of hoisting drum
(22)
being  md 
2
Clearly, V2  0 for every positive definite matrix,
  diag 1 ,  2  . Applying Barbalat’s lemma, we easily
638
 l0  ld 180
 rm
 528.880  1.469 revolutions.
16th Asia Pacific Vibration Conference
24-26 November, 2015
HUST, Hanoi, Vietnam
APVC2015
back-stepping SMC based responses is faster and smoother
than that of conventional SMC base responses. Although
controllers (26) and (37) can not completely stabilize the
ship responses, they partly reduce heave and roll motions
of ship as shown in Figs 8b&9b. We can see obviously in
Figs 8b&9b that back-stepping SMC based ship responses
are better than conventional SMC based ship responses.
Notably, the main duty of proposed controllers is to
stabilize responses of the container crane. The solution for
ship stabilization is not included in proposed controllers
(26)&(37). Normally, stabilizing the ship rely on naval
architectural engineering which has not been mentioned
here.
Table 1. System parameters and gains of controllers
Conventional
Back-stepping
System parameters
SMC
SMC
1  0.2,
1  0.2,
 2  0.4,
 2  0.3,
1  13,
1  13,
 2  1,
 2  0.1,
3  4,
3  3,
 4  0.1,
 4  0.1,
K1  K 2  2,
1   2  5,
40
30
Displacement (m)
a2 = 32 m, a3 = 12.5
m, a4 = 12.5 m,
rm = 0.325 m, l0 =15
m, mb = 4500000 kg,
mt =5900 kg, mc =
650 kg, Jb =
571875000 kgm2,
Jm = 41700 kgm2, k1
= 1250000 N/m,
k2 = 1250000 N/m, k3
= 12000 N/m,
b1 = 200 Ns/m,
b2=200 Ns/m, b3 =
220 Ns/m,
bt = 50 Ns/m, g =
9.81m/s2, bm = 70
Ns/m.
20
10
0
The duties of controllers (10) and (21) are strictly
complicated since only two control inputs are applied to
drive six system outputs. The initial conditions correspond
to static balance of crane-ship system given by
(25)
q1  0   q2  0   q3  0   q 4  0   q5  0   q6  0   0
(26)
(  max  46 , smax  3.8 cm )
1.5
2
2.5
Time (s)
3
3.5
4
Conventional SMC
Backstepping SMC
3
2
1
0
0
10
20
30
40
50
Time (s)
Fig. 3b. Trolley motion (xt): Conventional and
back-stepping controls
0.2
The number of revolutions
amplitudes
1
4
(iii) Simulation results and analysis. The simulation
results are described in Figs. 3-9. Without control, trolley
motion is destabilized (Fig. 3a). Conversely, the proposed
controllers precisely track the trolley moving to 3m-desired
position (Fig. 3b). In the case that control strategy is not
equipped, the axial oscillation of container (Fig. 7a) and
container swing (Fig. 6a) trend to divergence with the large
0
0.5
Fig. 3a. Trolley motion (xt): Uncontrolled case
Displacement (m)
q1  0   q2  0   q3  0   q4  0   q5  0   q6  0   0
0
Furthermore,
container cannot be lifted to reference (Figs. 4a&5a). The
instability of container crane partly leads the ship to
instable motions (Figs. 8a&9a). The conventional SMC and
back-stepping SMC make the responses of container crane
asymptotically approach to references: container is lifted to
12 m – desired cable length (Fig. 5b) within 18 sec,
0.15
0.1
0.05
0
-0.05
0
10
20
30
40
50
Time (s)
container swing is kept small (  max  1.40 ) during the
Fig. 4a. Rotation of hoisting drum (m): Uncontrolled case
transportation period and absolutely suppressed at its
destination (Fig. 6b). The axial container oscillation due to
elasticity of cable (Fig. 7a) is completely eliminated by
proposed controllers within 9 sec as seen in Fig 7b. It can
be seen in Figs. 4a&5a that the convergence of
639
16th Asia Pacific Vibration Conference
24-26 November, 2015
HUST, Hanoi, Vietnam
APVC2015
1.5
Conventional SMC
Backstepping SMC
1.5
1
0.5
0
Conventional SMC
Backstepping SMC
1
Angle (degree)
The number of revolutions
2
0.5
0
-0.5
0
10
20
30
40
-1
50
0
10
20
Time (s)
30
40
50
Time (s)
Fig. 4b. Rotation of hoisting drum (m): Conventional and
back-stepping controls
Fig. 6b. Container swing (): Conventional and
back-stepping controls
0.06
15.2
15
14.8
14.6
14.4
0.04
Displacement (m)
Cable length (m)
15.4
0.02
0
-0.02
0
10
20
30
40
50
-0.04
Time (s)
0
10
20
Fig. 5a. Container-lifting motion: Uncontrolled case
50
Conventional SMC
Backstepping SMC
14
0.03
13
Displacement (m)
Cable length (m)
40
Fig. 7a. Axial container oscillation (s): Uncontrolled case
15
12
11
30
Time (s)
0
10
20
30
40
50
Conventional SMC
Backstepping SMC
0.02
0.01
0
-0.01
Time (s)
Fig. 5b. Container-lifting motion: Conventional and
back-stepping controls
-0.02
0
5
10
Time (s)
15
20
Fig. 7b. Axial container oscillation (s): Conventional and
back-stepping controls
60
5
20
4
0
Displacement (m)
Angle (degree)
40
-20
-40
-60
0
10
20
30
40
50
3
2
1
0
Time (s)
Fig. 6a. Container swing (): Uncontrolled case
-1
0
10
20
30
40
Time (s)
50
60
Fig. 8a. Ship heave (y): Uncontrolled case
640
70
16th Asia Pacific Vibration Conference
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HUST, Hanoi, Vietnam
APVC2015
6. References
0.08
Conventional SMC
Backstepping SMC
Displacement (m)
0.06
(1)
0.04
0.02
(2)
0
-0.02
-0.04
0
10
20
30
40
Time (s)
50
60
70
Fig. 8b. Ship heave (y): Conventional and back-stepping
controls
(3)
5
Angle (degree)
0
(4)
-5
-10
-15
-20
-25
(5)
0
10
20
30
40
Time (s)
50
60
70
Fig. 9a. Ship roll (b): Uncontrolled case
Angle (degree)
0.02
Conventional SMC
Backstepping SMC
0
(6)
-0.02
(7)
-0.04
-0.06
0
10
20
30
40
(8)
50
Time (s)
Fig. 9b. Ship roll (b): Conventional and back-stepping
controls
(9)
5. Conclusion
(10)
Based on conventional SMC and back-stepping
integrated SMC techniques, two robust nonlinear
controllers was proposed to control the outputs: tracking
the trolley to desired position, hoisting the payload to
reference cable length, suppressing the container swing,
eliminating the axial oscillation of container along the
cable, and reducing the vertical oscillation and the roll
angle of ship. The controllers were designed for the
complicated operation of container crane-ship system in
which the effects of viscoelasticity of seawater and
elasticity of hoisting cable was fully considered. The
simulation results show that the container crane’s responses
are asymptotically stabilized and ship’s vibrations were
considerably reduced.
(11)
(12)
(13)
(18)
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642
AUTHOR INDEX
Last, Firstname
Page
A
Abdulkareem, Muyideen
170
Abe, Akira
668
Ahn, Byung-Hyun
555, 855
Ahn, Hyeong-Joon
516, 546,
702, 780
Dinh, Gia Ninh
268
Dinh, Tan Hung
183
Hongu, Junichi
708
Dinh, Van Phong
532, 799
Horii, Hirosuke
93
Do, Dang Khoa
532, 784
Horiuchi, Makoto
395
730
Hosokawa, Kenji
77
Do, Nam Duc
Do, Sanh
532, 784
844
Duong, Ngoc Khanh
552
Huang, Xianzhen
538
Huang, Zhicheng
191
Andou, Hiroaki
606
F
Aoki, Takashi
725
Fan, Chao
588
Aoki, Yasuo
725
Fang, Yuhong
368
149
Aono, Akihiro
37
Fujimoto, Shigeru
Aoshima, Keita
342
Fujita, Katsuhide
Asami, Toshihiko
324
Fujita, Satoshi 103, 108, 232, 500,
Asaoka, Sho
149
679, 686
Aziz, Z.A.
286
571
Brown, Terry
560
Bui, Huy Kien
268
Byon, Jun Ho
99
Caracoglia, Luca
300, 391
154, 162
Ikeda, Toshiyuki
406
Inami, Kimihiko
686
Furuya, Nobuyuki
Furuya, Osamu
93
149, 177, 494
G
Goda, Kengo
494
Ha, Jung-Min
555
588
Hase, Yuki
500
Cheng, Li
42, 844
Hasebe, Yusuke
361
Cho, Chung Il
546, 780
Hayashi, Toshiya
69
Choi, Byeong-Keun
386, 491,
Hee, L. M.
555, 855
Hemmati, Hossein
714
708
806
93, 222
Chen, Ye
Dao, Duy Lam
Iba, Daisuke
Imran, Sardar Muhammad
Furuya, Kohei
448
336
I
324
Han, Qinkai
Dang, Bao Lam
516, 702
Imanishi, Kazuya
456
D
Hwang, Kang-Jo
718
Chen, Lumiao
191, 448, 456
435
Furuya, Keiichiro
Han, Jae-Hung
Chu, Fulei
Hwang, Jae Deok
Imamura, Kyosuke
440
435
521, 525
113
Chen, An-jun
Choi, Hun Oh
Hui, K. H.
Fukui, Kotaro
H
C
806
Huang, Wei
295
Bangchun, Wen
Hou, Zhichao
374
Akao, Satoru
170
760, 886
Duong, Ngoc Hao
99
Bakhary, Norhisham
69, 87, 212, 655,
268
Ahn, Jin Ho
B
Honda, Shinya
Dao, Huy Bich
461, 512
525
63
Hino, Junichi
754
Hirai, Takao
837
Hisano, Shotaro
878
Hoang, Manh Cuong
633
Hoang, Phuong Hoa
244
32
Inoue, Takumi
131, 871
Ise, Tomohiko
324
Ishihana, Kenta
494
Ishihara, Yukiko
232
Ishikawa, Satoshi
142, 506, 878
Ishizuka, Shinichi
718
Isoda, Ryosuke
307
Itadani, Kota
312
Ito, Akihito
54, 468, 606
Ito, Norihisa
860
Ito, Tomohiro
329
Itoga, Takaaki
324
Iwamoto, Hiroyuki
126, 694
Iwasaki, Makoto
860
Izyan, M.D. Nurul
286
J
Jang, Kuehwan
823
Jang, Yong-Ho
491
Jeong, Jae Seong
516, 780
Kosaka, Fumihiko
395
Mori, Yoshifumi
Jeong, ManYong
342, 352
Kozukue, Wakae
601
Morishita, Shin
Jeong, Sin Woo
Ji, Hongli
228
42, 844
Kumagai, Takahito
Kunimatsu, Yuki
391
295, 361
Morita, Yoshifumi
860
318
Moriwaki, Ichiro
708
606, 837
Mukai, Yasuhiko
860
87
Ji, J.C.
560
Kuratani, Fumiyasu
Jiang, Huan-xin
440
Kuroda, Katsuhiko
237
Muramatsu, Ken
149
Jiang, Jing
593
Kwon, Chang-Beom
512
Muta, Hitoshi
149
N
L
K
La, Duc Viet
623
Na, Sungsoo
823
131, 871
Le, Anh Tuan
633
Nagamine, Takuo
690
Kaito, Yoshihiko
886
Le, Thai-Hoa
154, 162
Nagatani, Asahiro
54
Kajiwara, Itsuro
718
Lee, Dong-Kyu
512
Nahvi, Hassan
63
Kamei, Junya
831
Lee, J.H.
286
Nakae, Takashi
Kaneko, Mitsugu
300
Lee, Jong Myeong
491
Nakagawa, Chihiro
329
Kaneko, Shigehiko
427
Lee, Jong-Myeong
386
Nakamura, Morimasa
708
Kano, Ryo
860
Lee, Joong Hyeok
99
Nakamura, Takenori
391
Kato, Masaki
113
Lee, Sang Jeong
59
Nakamura, Tomomichi
Kato, Ryo
679
Leong, M. Salman
Kabune, Hideki
860
Kadowaki, Ren
Kawamura, Shozo 32, 37, 54, 307,
312, 395
521, 525
475, 614
6
Nakano, Takahiro
871
Li, He
582
Nakano, Yutaka
380
Li, Hui
582
Nanba, Akihiro
475
Kawashima, Takeshi
419
Liang, Jack
566
Narita, Yoshihiro 69, 87, 212, 655,
Kijimoto, Shinya
878
Lim, M. H.
521
760, 886
Kim, Byeonghee
99
Liu, Panxue
538
Nariya, Koji
108
Kim, Chae Sil
435
Liu, Shuying
593
Nerse, Can
218
Kim, Dong Il
435
Liu, Ziliang
576
Ngo, Kieu Nhi
Lu, Li-xin
440
Ngui, W. K.
521, 525
Nguyen, Anh Tuan
461, 643
Kim, Hack-Eun
386, 491
Kim, Hyo Jung
491, 855
Kim, Kihyun
1
Kim, Kwang-Joon
81
Kim, OeCheul John
855
Kim, Seockhyun
99
Kim, Yong-Seok
555, 855
Kishida, Takuya
131
Koba, Yosuke
878
Kobayashi, Koji
860
Kobayashi, Takanori
690
Koike, Yoshio
136
Koketsu, Yu
406
Kondou, Takahiro
142, 506,
662, 673
M
Matsubara, Masami
32, 37, 54,
307, 312, 395
Matsuda, Tomoyuki
204, 730
Matsumura, Yuichi
93, 222
Matsuoka, Taichi
Matsuzaki, Kenichiro
400
142, 475,
506, 614, 673
Minagawa, Keisuke 103, 232, 500,
679, 686
Miura, Nanako
204, 730
Miyaji, Hideyuki
601
Mizota, Toru
673
Mori, Hiroki
673, 690
13, 21, 738, 746
Nguyen, Ba Nghi
623
Nguyen, Ba Tuyen
222
Nguyen, Canh
516
Nguyen, Cao Thang
374
Nguyen, Da Thao
13
Nguyen, Dinh Duc
251
Nguyen, Dinh Dung
791
Nguyen, Dong Anh
374, 413
Nguyen, Duc Thi Thu Dinh
278
Nguyen, Duc-Canh
702
Nguyen, Duy-Thao
767
Nguyen, Hung Chi
730
Nguyen, Huu Hung
119, 278
Nguyen, Ngoc Linh
413
Park, Youngjin
826
Son, Seok-Man
Sone, Akira
Nguyen, Quang Hoang
791, 799
Pham, Anh Duc
546
Nguyen, Quang Thanh
13, 21
Pham, Bao Toan
13, 21
555
204, 730
Sonobe, Motomichi
754
Nguyen, Sy Dzung
738, 746
Pham, Dinh Trung
244
Sowa, Nobuyuki
673
Nguyen, Toan Xuan
196, 260
Pham, Minh Hai
336
Sudo, Mutsuhito
686
244
Pham, Thai Quoc
329
Sueoka, Atsuo
Nguyen, Van Khang 643, 649, 791
Pham, Van Trieu
633
Sumitani, Takuya
Nguyen, Van Quyen
799
Phan, Dang Phong
784
Suzuki, Yuto
Nguyen, Van Sy
183
Nguyen, Vien Quoc
746
Nguyen, Viet Trung
278, 714
Nguyen, Trong Phuoc
Nguyen, Xuan Ha
Nguyen, Xuan Thuan
336
Qiu, Hengbin
Qiu, Jinhao
191, 456
483
42, 844
204, 730
Nguyen, Xuan-Toan
767
Niikawa, Takeshi
113
Niiyama, Nobuhiro
177
Nishida, Seiji
860
Nishioka, Fumiya
760
Niwa, Tomonori
400
R
Ren, Zhaohui
582
Roh, Woo-Jin
59
Rosbi, Sofian
475, 614
Roser, Holger
368
Ryu, Homin
Ryu, Takahiro
1
475, 614
O
Oda, Tatsuya
Ogata, Keiji
Ogushi, Masaki
Oh, Yutaek
Ohama, Kazumasa
Ohashi, Tatsuro
Ohmata, Kenichiro
Ohmura, Kazuhisa
Okabe, Keisuke
Okamoto, Mineki
Omata, Shohei
Ooi, Yoichi
871
177
850
50
131
77
400
131
668
774
494
475, 614
P
Park, Chanho
823
Park, Gyu-Jin
386
Park, Jinsung
823
Park, Jong-beom
59
Park, No-Cheol
59
Park, Sun Hwi
491
Park, SunHwi
855
S
Saito, Takashi
295
Sanada, Akira
866
Sasajima, Manabu
136
Sasaki, Takayuki
708
Sasuga, Masashi
93
Sato, Hiroki
468
Sato, Yuichi
690
Seo, Tae Il
352
Ta, Tuan Hung
552
Tagawa, Yasutaka
725, 774
Takahara, Hiroki
380
Takahashi, Osamu
108
Takai, Akihiro
427
Takayanagi, Tenma
400
Takehara, Shoichiro
318, 406
Takikawa, Yoshihiro
475, 614
Tampo, Tatsuya
212
Tanaka, Go
679
Tanaka, Motoki
817
Tanaka, Nobuo 126, 694, 817, 866
300, 391
Sakurai, Tomoki
Seo, Soon-woo
6
T
Q
Qin, Zhaoye
475, 614
81
738, 746
Shida, Zenichiro
406
Shimura, Yuta
103
Shin, Min Jae
435
Shintani, Atsuhiko
329
Shiohata, Koki
850
Shiozaki, Hirotaka
222
Shiraishi, Toshihiko
361, 831
Shirasuna, Noriyuki
380
Shuying, Liu
571
Son, Daehyuk
826
Tanaka, Soichiro
655
Tanaka, Yudai
108
Tang, Liling
42
Taniguchi, Tomoyuki
662
Terumichi, Yoshiaki
318, 406
Tran, Duc
532
Tran, Duc Van
196, 260
Tran, Ngoc An
649
Tran, Quang Thinh
738
Tran, Quoc Quan
251
Tran, The Linh
546
Trieu, Quoc Loc
643
Truong, Nang Toan
746
Tsujiuchi, Nobutaka
54, 468, 606
V
Vafaei, Mohammadreza
170
Viswanathan, K.K.
286
Vo, Van Huong
552
Vu, Dinh Quy
28, 183
Vu, Duc Binh
784
W
Walker, Paul
368
Wang, Hao
538
Wang, Jun
440
Wang, Qi-li
440
Wang, Semyung
1, 218
Washio, Saiji
837
Watanabe, Mitsuharu
136
Watanabe, Motoya
694
Watanabe, Seiji
113
Wen, Bangchun 576, 582, 588, 593
Wu, Yan
593
X
Xu, Xueping
448
Xu, Zili
483
Xueliang, Zhang
571
Y
Yamada, Joji
6
Yamaguchi, Hirotaka
754
Yamaguchi, Takao
136
Yamashita, Masashi
628
Yamazaki, Daisuke
361
Yang, Zhou
538
Yao, Hongliang
576
Yoo, Hong Hee
50, 228
Yoon, Jae-San
512
Yoshida, Kazuhiro
177
Yoshida, Tatsuya
606, 837
Yoshida, Yuto
318
Yoshidomi, Mami
468
Yoshitake, Tatsuhiro
142
You, Junseok
823
Yu, Hyeon-Tak
386
Z
Zakaria, M. K.
525
Zhang, Chunmei
483
Zhang, Nong
Zhang, Su
368, 566
42
Zhang, Yimin
538
Zhao, Chunyu
588
Zhu, Sangzhi
566
Zongyan, Wang
571
Proceedings of the 16th Asia Pacific Vibration Conference.
Bach Khoa Publishing House, Hanoi
1 – Dai Co Viet – Hanoi
Tel. (84.4) 3868 4569; Fax. (84.4) 3868 4570
http://nxbbk.hust.edu.vn
-----***-----
Responsible for Publication
Director and Editor-in-Chief: Dr. Phung Lan Huong
Technical Editors: Nguyen Quang Hoang
Nguyen Van Quyen
Tran Ngoc Huan
Produced at: Bach Khoa Publishing House, Hanoi,
01 Dai Co Viet Street, Hai Ba Trung District, Hanoi.
Quantity: 300 CD.
Registration No.: 3317 – 2015/CXBIPH/02 – 83/BKHN.
ISBN: 978-604-938-726-5.
Archived: IV – 2015.
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