Underwater Sound Radiation Control by Active Vibration Isolation an Experiment

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    Engineers, Part M: Journal of Engineering forProceedings of the Institution of Mechanical

    http://pim.sagepub.com/content/223/4/503The online version of this article can be found at:

    DOI: 10.1243/14750902JEME157

    223: 5032009oceedings of the Institution of Mechanical Engineers, Part M: Journal of Engineering for the Maritime Environment

    Z Zhang, X Huang, Y Chen and H HuaUnderwater sound radiation control by active vibration isolation: An experiment

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    Underwater sound radiation control by active vibrationisolation: an experimentZ Zhang*, X Huang, Y Chen, and H Hua

    State Key Laboratory of Mechanical Systems and Vibration, Shanghai Jiaotong University, Shanghai, Peoples Republic

    of China

    The manuscript was received on 14 February 2009 and was accepted after revision for publication on 29 June 2009.

    DOI: 10.1243/14750902JEME157

    Abstract: An experimental system, mainly including a rotary machine, four active vibrationisolators and a water container, was established to investigate the role of active vibration

    isolation in suppressing vibration transmission as well as underwater sound radiation. Finiteelement analysis and experimental modal testing were employed to exhibit and validatevibration modes of the fluid-coupled structure and the radiated sound field in water. Soundfield given by this validated finite element model is taken as the substitution for a realmeasurement. In the experiment, the fundamental frequency of the rotary machine was chosento be nearly equal to a natural frequency of the coupled system in order to create a sound fieldin the water container by resonant structural vibration. The rotary machine is supported by thefour electromagnetic vibration isolators, which suppress the quasi-periodical local vibrationindependently according to an adaptive control method. The measured results havedemonstrated that low-frequency sound radiation can be reduced by local active vibrationisolation.

    Keywords: active vibration isolation, underwater sound radiation, fluidstructure interaction,

    adaptive control

    1 INTRODUCTION

    Fluidstructure interaction and the pertinent sound

    radiation have been thoroughly investigated since

    the 1950s, but the research on active control of

    sound radiation started very late. Compared with the

    abundant work in the active control of structure-

    borne sound in the air, there is scant research

    concerning active control of vibration and/or sound

    radiation from structures in heavy fluid [13].

    However, structures filled with and/or surrounded

    by heavy fluid are frequently met in applications, for

    example, in the area of ship transportation. Vibration

    of ship structures induced by power machinery is

    harmful to passengers as well as the ocean environ-

    ment, especially the vibration at low frequencies,

    usually less than several hundred Hertz, is difficult to

    control by passive means. Active isolation of vibra-

    tions of power machinery is an effective means to

    reduce vibration transmission and hence the sound

    radiation of structures. There is plenty of research on

    active vibration isolation, concerning control algo-

    rithms as well as implementation [46]. Vibration of

    structures is strongly influenced by heavy fluid at

    low frequencies. The added inertia effect of fluid

    clearly changes the natural vibration frequencies of

    structures and, accordingly, the radiation of sound.

    Therefore, fluidstructure interaction should be

    considered in the control of low-frequency vibration.

    Currently, the commonly used methods in describ-

    ing fluidstructure interaction are the finite element

    method (FEM) and/or the boundary element

    method (BEM). The FEM/BEM methods are superior

    in analysing structures coupled with unbounded

    domain of fluid [79]. For the analysis of steady-state

    structural vibration and sound radiation, the

    coupled motion is usually given in the frequency

    domain with fluid compressibility taken into ac-count. However, it is more flexible to apply a time

    *Corresponding author: State Key Laboratory of Mechanical

    Systems and Vibration, Shanghai Jiaotong University, Shanghai,

    Peoples Republic of China.email: [email protected]

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    domain model in simulation and to investigate non-

    linearity in active vibration control. In order to carry

    out active vibration isolation in real time, a lower

    order model that describes the fluidstructure inter-

    action with sufficient accuracy is necessary. The

    validated numerical model (modal model) and the

    directly measured model are appropriate to real-

    time control and the latter is preferable in practice

    and is adopted in this paper.

    Adaptive cancellation is one of the adaptive

    strategies that can cancel periodic disturbances

    and is used widely in many fields, such as signal

    processing as well as control engineering. In active

    vibration isolation, cancellation with tracking filters

    can suppress tonal vibrations at specified frequen-

    cies, but needs online frequency estimation since the

    centre frequencies of these filters are adjustedaccording to disturbing forces/moments. Filtered-x

    least mean squares (FxLMS) and recursive least

    squares are important adaptive control algorithms

    and, especially, FxLMS is often used in real applica-

    tions owing to its fast computation and easy imple-

    mentation. In noise cancellation, FxLMS is used

    independently or combined with tracking filters to

    control harmonic sound [1012]. FxLMS can also be

    applied in the control of low-frequency vibration of

    thin plates, where the vibration control involves

    fluidstructure interaction [3]. In the control of

    engine-induced mount vibration, the multi-channelactive vibration isolation scenario with FxLMS has

    achieved notable reduction in vibration [4]. In the

    FxLMS algorithm, controller weights are updated

    according to error signals and a large disturbance in

    the error will lead to excessive adaptation of weights,

    which can cause saturation in the controller output

    and consequently deteriorate control performance.

    For active vibration isolation, saturation will cause

    high-frequency vibrations and even resonance in an

    isolation system. However, controller saturation in

    active vibration isolation has been rarely concerned

    [13]. Non-linearity in vibration isolation is compli-cated and is usually related to a particular problem.

    In this paper, active vibration isolation and its

    influence on the underwater sound field in a

    plexiglass water container are discussed by an

    experiment, which is the subsequent work of an

    early investigation by the authors [9]. The work

    demonstrates the effectiveness of active isolation in

    the attenuation of sound radiation as well as the

    influence of vibration modes to the radiated sound

    field. Before conducting the experiment, FEM is first

    employed to analyse the coupled vibration andexhibit underwater sound field corresponding to

    the natural vibration modes. The numerical model

    and results are used to explain the controlled sound

    field. In the implementation of active vibration

    isolation, the adaptive controller is embedded with

    tracking filters. The role of tracking filters is to track

    vibration signals of oscillating frequencies. More-

    over, saturation in controller output is alleviated by

    compressing the updating of weights of the adaptive

    controller and accordingly a good performance of

    active isolation in the presence of abnormal dis-

    turbances can be expected [14].

    Detailed discussion is given in five sections. Finite

    element analysis and model validation are given in

    section 2; section 3 gives a short discussion on the

    adaptive control algorithm; Experimental results are

    presented in section 4, and conclusions are pre-

    sented in section 5.

    2 ANALYSIS AND VALIDATION OF THEEXPERIMENTAL MODEL

    For the analysis of interaction between structures

    and fluid within a finite space, the finite element

    method is usually an appropriate choice since the

    vibration displacements and sound pressure can be

    described by a discrete model of finite degrees of

    freedom. The natural vibration modes of the coupled

    system are then obtained by solving matrix eigen-

    value problems [15]. The purpose of numerical

    analysis is to exhibit sound field in the water, which

    is usually easy to simulate but difficult to measure.

    One part of the experimental model is the

    plexiglass water container with a plexiglass plate

    installed on its top, as shown in Fig. 1. The wall

    thickness of the container is 50 mm and its dimen-

    sions are 60067006800 mm (height). The plate is

    20 mm thick and the dimensions of the surface in

    contact with water are 3006600mm. In the finite

    element model, the container is modelled with 8512

    solid elements, the plate with 296 shell elements and

    the water with 23 013 fluid elements. Mechanical

    properties of the materials are listed in Table 1.

    The coupling between the container and water is

    on the five interfaces where the container contacts

    the water. The top surface of the water is partly

    coupled with the plate and there are two separate

    free water surfaces. In the computation, the pressure

    on the free surfaces is set to zero (The effect of air is

    neglected and the coupled system is assumed to

    vibrate in vacuo). The model without water is first

    analysed, and the first four natural frequencies of the

    dry plate are listed in Table 2, in which thecomputed results and the measured results obtained

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    by modal testing are very close. Then, the model

    with water is analysed and the first four natural

    frequencies of the wet plate are also listed in Table 2.

    As can be seen, the computed frequencies are again

    close to the measured ones. In Table 2, all the

    frequencies of the plate clearly decrease after it is

    coupled with the water, which implies a strong

    interaction between the plate and the water. Figure 2

    gives the first four mode shapes of the plate coupled

    with water. In these mode shapes, the first and the

    third are bending modes and the second and the

    fourth are torsional modes. Pressure distributions

    corresponding to the four natural modes are shown

    in Fig. 3. As can be seen, the distribution is closely

    related to a vibration mode and the maximum

    pressure corresponds almost to the largest ampli-

    tude of the mode shape.The finite element model was validated by modal

    testing. Apart from the natural frequencies, mode

    shapes of the plate in the coupled system were also

    measured. Figure 4 gives the measurement points as

    well as the measured mode shapes. The location of

    these points is determined on the basis of computed

    mode shapes in order fully to exhibit the node lines

    as well as the peak lines. Compared with the shapes

    in Fig. 2, the measured shapes have almost the same

    peak and node lines.

    As the model is validated, one can obtain a

    reasonable pressure field in the water container byanalysis. Figures 5(a) and 6(a) are slices of pressure

    distribution corresponding respectively to the first

    and second natural vibration modes of the plate. The

    two slices are at the same location, 150 mm away

    from the inside wall surface of the container. In the

    slice, 12 observation points are selected, among

    which the first three points are near the free surface

    and the rest are located 100500 mm below the free

    surface with even distance of 50 mm. By dividing the

    pressure at every point by the maximum pressure,

    one can give normalized values to each point.

    Figures 5(b) and 6(b) show the variation of thenormalized values of the 12 points with respect to

    the depth. It can be seen from the two figures that

    sound fields to the first two vibration modes are

    distinct. The sound pressure induced by the first

    mode is distributed globally while that by the second

    mode is distributed locally. This difference is

    attributed to the different radiation directivity of

    vibration modes. For the first mode, every point on

    the plate vibrates in phase, but for the second mode,

    any two points located symmetrically about the

    node line vibrates out of phase, resulting in strongdirectivity in the field.

    Fig. 1 The water container, plate and water: (a) topview; (b) without water (unmeshed); (c) with

    water (meshed)

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    The overall experimental system is shown in

    Fig. 7. As can be seen, the container is almost full

    of water, which contacts the lower surface of the

    plexiglass plate. Four active isolators are installed

    between the plexiglass plate and an aluminium plate

    with dimensions 3006

    1806

    8 mm. The fan, havingan eccentric mass, is used as a rotary machine and

    supported on the aluminium plate. Its nominal

    speed is 2400r/min and the nominal fundamental

    frequency is therefore 40Hz. The first natural

    frequency of the aluminium plate is about 466 Hz,

    much higher than this fundamental frequency as

    well as the first natural frequency of the plexiglassplate. The active isolators are electromagnetic

    Table 1 Mechanical properties

    Youngs modulus/bulkmodulus (N/m2) Density (kg/m3) Poissons ratio Sound speed (m/s)

    Plexiglass 3.956109 1200 0.35 Water 2.256109 1000 1500

    Table 2 Computed and measured natural frequencies of the plate

    No water in the container, active isolators not installed

    Computed (Hz) 70.3 134.8 213.5 318.3Measured (Hz) 71.40.5 137.50.5 209.20.5 314.0 0.5

    Container filled with water, active isolators not installed

    Computed (Hz) 28.3 79.0 85.6 190.6Measured (Hz) 29.00.5 78.40.5 89.20.5 186.2 0.5

    Container filled with water, active isolators installed

    Measured (Hz) 39.40.5 81.30.5 97.00.5 209.5 0.5

    Fig. 2 The first four mode shapes of the plate

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    actuators. Diameter and height of each actuator are

    50 and 40 mm respectively and the first natural

    frequency is 66Hz. Natural frequencies of the

    plexiglass plate are altered after the installation of

    active isolators, which are also measured and listed

    in Table 2. The table shows that each natural

    frequency becomes larger the first rises to

    39.4 Hz, but the second has only a small variation.

    Since the first natural frequency is very close to the

    fundamental frequency of the fan, the radiated

    sound exhibits a strong resonance at this frequency,

    as can be observed in the experiment. Theoretically,

    not only the natural frequencies but also mode

    shapes of the plate will change with the installation

    of active isolators, so will the induced sound field.

    However, the sound field to the first natural

    frequency is similar to that in Fig. 5 because the

    plexiglass plate in Fig. 7 can be regarded as a

    stiffened one by the actuators and the aluminium

    plate.

    In the experiment, four accelerometers are in-

    stalled beside the active isolators to measure the

    responses of the plexiglass plate and one acceler-

    ometer on the aluminium plate to measure the

    vibration of the fan. Moreover, one sound pressure

    transducer is immersed in water to measure the

    underwater sound pressure induced by the resonant

    vibration of the plexiglass plate. The controller is a

    PC with one NI-PCI6259 board inside, which has 32

    input channels and 4 output channels.

    3 ADAPTIVE METHOD IN ACTIVE VIBRATIONISOLATION

    The vibration induced by the rotating eccentric mass

    is composed of harmonics. For periodical responses,

    the control method adaptive cancellation is an

    effective way to counteract the influence of distur-

    bance. The adopted adaptive control system is

    shown in Fig. 8, where Hs(z) and Hc(z) are the

    transfer functions respectively from Fd and Fc to the

    vibration acceleration at point S. Fd and Fc represent

    respectively the disturbance force and the control

    force. In Fig. 8(b), the control force Fc is applied to

    cancel the vibration of S induced by the disturbance

    force Fd. The reduction of vibration at point S will

    result in a decrease of sound radiation from the plate

    structure. Adaptation of Fc is realized according to

    the vibration of point S, i.e. the error signal. The

    adaptive controller is constructed on the FxLMS

    algorithm. In the figure, F(z) represents tracking

    filters, Hc(z) is the estimate of Hc(z), W(z) the

    controller, d(k) the disturbance, e(k) the error signal,

    r(k) the reference signal, y(k) the response induced

    by u(k).

    The discrete transfer function ofF(z)

    shown inFig. 8(a) can be described by

    Fig. 3 Pressure distribution on the top surface of thewater

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    Fig. 4 The first four mode shapes of the plate (left measurement points; right mode shapes)

    Fig. 5 Sound field to the first vibration mode: (a) a slice of the sound field (normalized pressure);(b) normalized pressure versus depth

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    F z ~ F1 z , F2 z , , Fn z T,

    Fi z ~bi0zbi2z

    {2

    1zai1z{1zai2z{2, i~1*n 1

    where ai1~{2exp {fvi=fs cosffiffiffiffiffiffiffiffiffiffiffiffi

    1{f2p

    vi=fs

    , ai2~

    exp {2fvi=fs , bi0~1=2 1{ exp {2fvi=fs , bi25

    2bi0, fs is the sampling frequency. In the adaptive

    isolation, the centre frequencies vi of F(z) are

    estimated by online frequency estimators.

    For each adaptive controller Wi(z), the adaptation

    of its coefficients can be given by equation (2)according to the LMS algorithm

    wi kz1 ~wi k zmei k

    cz ri k k k2ri k

    u k ~P

    i

    wTi k ri k , i~1*n 2

    where ri(k) is the output of Hc(z) under the inputri(k), r(k)5 (r1(k),r2(k),...,rn(k))

    T, ei(k) the output ofFi(z) under the input e(k), m is an adjustingparameter, c. 0. However, in this paper, equation(2) is replaced by a modified formula.

    Since the control signal u(k) is the output of W(z)

    under the input r(k), and one step update of coeffi-cients of W(z) given in equation (2) is proportional

    Fig. 6 Sound field to the second vibration mode: (a) a slice of the sound field (normalizedpressure); (b) normalized pressure versus depth

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    to the filtered error signal ei(k), excessive adaptation

    will occur when there is a large shock in the error

    signal, which can result in saturation in controlleroutput. Output saturation can produce high-fre-

    quency excitation and even instability, which will

    deteriorate vibration isolation. Therefore, the adap-

    tation formula in equation (2) should be modified to

    consider this circumstance. For an ideal saturation

    sat u k ~

    d, u k wd

    u k , u k j jd

    {d, u k v{d

    8>: , dw0 3

    the following formula can be deduced by solving anoptimization problem [14]

    Fig. 7 Experimental system for active vibration isola-

    tion and underwater sound radiation control:(a) photograph; (b) front view; (c) top view

    Fig. 8 Active isolation and the adaptive controlscheme with tracking filters

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    wi kz1

    ~fu wTi k ri k

    wi k zmei k

    cz ri k k k2ri k

    !

    4

    where fu wTi k ri k

    is the derivative of a sigmoid

    function f(u) with respect to the variable u. Accord-

    ing to the definition of sigmoid functions, as u(k)

    approaches saturation, fu wTi k ri k

    decreases fast

    to zero and consequently reduce the adaptation

    step of wi(k). This property guarantees that

    fu wTi k ri k

    is able to weaken any excessive

    updating of wi(k) and alleviate output saturation.

    Moreover, equation (4) can degrade to equation (2)

    as long as no output saturation occurs.

    4 EXPERIMENTAL RESULTS

    Figure 9 is the measured fundamental frequency of

    the fan, which indicates that the rotation speed is

    not constant but oscillates between 40.5 and 41.1 Hz.

    In the figure, there are 4800 samples in total,

    corresponding to a 12 s record under the sampling

    frequency 400 Hz. Therefore, the oscillation fre-

    quency of the speed is very small as compared with

    the fundamental frequency. The given adaptive

    algorithm with real-time tracking filters is not

    sensitive to the variation of speed, which can

    guarantee a large attenuation of quasi-periodical

    vibrations even under unsteady excitation.

    Transfer functions from the control voltage to the

    local acceleration responses at the four active

    isolators are measured for further implementation

    of active isolation. Figure 10 gives the measured

    frequency response functions (FRFs), and the FRF

    from the control voltage of the second active isolator

    to the measured sound pressure at point 4 (marked

    in Figs 5 and 6) is also shown for comparison. The

    following conclusions can be drawn from these

    measured curves.

    1. FRFs of the four active isolators are almost the

    same except at the natural frequencies.2. In the pressure/voltage curve, all peaks corre-

    spond to the natural frequencies of the plate as

    well as the active isolators, and at the observation

    point, sound pressure induced by the second

    mode (at 81 Hz) is stronger than the other three

    modes of the plate.

    3. When excited by white noise, natural vibration of

    the active isolators will create higher sound

    pressure than the first four modes of the plate,

    which implies that the natural vibration should be

    damped in the implementation of active isolation.

    With the measured FRFs of active isolators and the

    adaptive control structure shown in Fig. 8, active

    control is implemented and each active isolator

    generates cancelling forces according to the local

    vibration accelerations to counteract vibration

    caused by the rotating fan and the corresponding

    radiated sound. Since the excitation of the fan is

    mainly composed of vibration at the fundamental

    frequency and forces the plate to vibrate resonantly

    at its first natural frequency, the spectrum of

    radiated sound from the plate at the fundamental

    frequency is dominant when no control is imple-mented. After active control, the radiation at the

    fundamental frequency is suppressed substantially,

    as shown in Fig. 11, where the spectrum at the first

    natural frequency of the isolator (about 66 Hz) is

    raised to some extent. In the resonant condition, the

    pressure at those points shown in Fig. 5 was

    measured and the results are given in Table 3, from

    which one can see that the trend implied by the

    pressure-depth data is similar to that shown in

    Fig. 5.

    Figure 12 gives the acceleration responses at the

    foot of the second active isolator before and after

    Fig. 9 The fundamental frequency of the fan

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    active isolation respectively, from which it can be

    seen that vibration at the fundamental frequency

    (around 40.8 Hz) is suppressed by 90 per cent, but

    increases at the second and the fifth harmonic

    frequencies (near 81, 205 Hz), and clearly rises at

    the first natural frequency of the isolator (about66 Hz). Comparing Fig. 12 with Fig. 11, it can be seen

    that the spectra of sound pressure at the second and

    fifth harmonic frequencies keep almost the same

    except at around 66 Hz, which increases by almost

    20 dB. Nevertheless, the total vibration and sound

    are attenuated by a large percentage. The reason for

    this phenomenon is that the radiated sound field atabout 81 or 205 Hz has strong directivity and the

    Fig. 10 Measured FRFs of the control channels: (a) acceleration versus voltage; (b) pressureversus voltage

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    measurement point is not in the radiation direction,

    which renders the measured sound pressure insen-

    sitive to the variation of vibration of the plate. The

    directivity is closely related to forced vibration

    modes of the plate, and the two vibration modes at

    81 and 205 Hz are actually similar to those given in

    Fig. 5.

    5 CONCLUSION

    Active vibration isolation and sound radiation of an

    experimental system with fluidstructure interaction

    are discussed. The vibration characteristics of the

    plate coupled with water in a plexiglass container areanalysed by the FEM and validated by modal testing,

    which forms a base for the explanation of controlled

    sound radiation in the water container. Active

    vibration isolation is realized on the basis of an

    adaptive algorithm with embedded tracking filters

    that are used to ensure the control process insensi-

    tive to the fluctuation of vibration frequencies. Four

    actuators operate independently to cancel local

    vibrations at each active isolator. The vibration and

    radiated sound at the fundamental frequency are

    suppressed substantially after active isolation. At

    certain high-order harmonic frequencies, vibration

    of the plate increases but results in indiscernible

    change in sound pressure. The radiated sound field

    is closely related to vibration modes, those modes ofstrong directivity in radiation induce only local

    Fig. 11 Sound pressure before and after control (Ref5161026 Pa and depth 5 500 mm):(a) time domain responses: (b) spectra

    Table 3 Sound pressure at different locations (Hanning window and linear average)

    No. 1 2 3 4 5 6 7 8 9 A B C

    Depth (mm) 5 10 25 100 150 200 250 300 350 400 450 500Sound pressure (Pa) 3.4 10.2 29.8 97.9 103.3 102.1 102.9 103.9 101.6 101.2 99.6 99.0

    Underwater sound radiation control by active vibration isolation 513

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    radiation, having weak influence on the sound

    pressure at locations away from the radiation

    direction, which usually cause a discrepancy in the

    attenuation of vibration and sound at certain

    harmonic frequencies after active isolation.

    ACKNOWLEDGEMENT

    This work was fully supported by the NSF of China(Grant No. 10672099).

    F Authors 2009

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    APPENDIX

    Notation

    ai1, ai2, bi0,

    bi0, bi2

    coefficients of the ith tracking

    filterd(k) disturbance

    e(k) error signal

    fs sampling frequency

    f(u) sigmoid function

    Fd, Fc disturbance force, control force

    F(z)5 (F1(z),

    F2(z),...,Fn(z))T

    tracking filters

    Hc(z), Hs(z) transfer functions

    Hc(z) estimate of Hc(z)

    r(k)5 (r1(k),

    r2(k),...,rn(k))T

    reference signals

    u(k) control signal

    wi(k) weight vector of the ith controller

    W(z)5 (w1(z),

    w2(z),...,wn(z))T

    controller

    y(k) response signal induced by u(k)

    ei(k) output of Fi(z)

    m, c. 0, d. 0 scalar variables

    ri(k) output of Hc(z)

    vi centre frequency

    Underwater sound radiation control by active vibration isolation 515

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