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  <front>
    <journal-meta />
    <article-meta>
      <title-group>
        <article-title>Numerical Damping of Vibrations of a Moving String</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>Igor E. Mikhailov</string-name>
          <email>igor@mail.ru</email>
          <email>mikh igor@mail.ru</email>
          <xref ref-type="aff" rid="aff0">0</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Ivan A. Suvorov</string-name>
          <email>ivan.a.suv@gmail.com</email>
          <xref ref-type="aff" rid="aff2">2</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Copyright ⃝c by the paper's authors. Copying permitted for private and academic purposes.</string-name>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Federal Research Center, \Informatics and Control" RAS</institution>
          ,
          <addr-line>Vavilov street, 44/2, 119333 Moscow</addr-line>
          ,
          <country country="RU">Russia.</country>
        </aff>
        <aff id="aff1">
          <label>1</label>
          <institution>In: Yu. G. Evtushenko, M. Yu. Khachay, O. V. Khamisov, Yu. A. Kochetov, V.U. Malkova, M.A. Posypkin (eds.): Proceedings of</institution>
          ,
          <addr-line>the OPTIMA-2017 Conference, Petrovac, Montenegro, 02-Oct-2017, published at http://ceur-ws.org</addr-line>
        </aff>
        <aff id="aff2">
          <label>2</label>
          <institution>Moscow Aviation Institute</institution>
          ,
          <addr-line>Volokolamskoe shosse, 4, 125993 Moscow</addr-line>
          ,
          <country country="RU">Russia.</country>
        </aff>
      </contrib-group>
      <fpage>406</fpage>
      <lpage>411</lpage>
      <abstract>
        <p>The basis of this research is the mechanical processes that take place in the production of paper. All papermaking machines contain open sections of the web between the support rollers. When the paper web moves, it may lose stability, break, or begin to make transverse vibrations. It is assumed that the amplitude of these vibrations is the same in the width direction of the web, so that the movement of the string in the axial direction with constant speed is considered as a model. It should be noted that because of the axial motion, the mechanics of moving materials are different from classical mechanics. In the paper, the decrease of vibrations is realized with the help of point-type actuators. The motion of the string is modeled by the initialboundary value problem for a partial differential equation of hyperbolic type, which is solved numerically by the method of characteristics. The vibration damping controlling actuators are modeled by the function on the right side of this equation. The problem is to damp the forced transverse vibrations of a moving string in a minimum time. Examples of calculations are given.</p>
      </abstract>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>-</title>
      <p>utt + 2V0uxt + (V02
c2)uxx = f (t, x),
0 6 x 6 l, 0 6 t 6 T,</p>
      <p>The initial disturbance
(1)
(2)
(3)
are known.</p>
      <p>Let us find a function f (t, x) from (1), that allows us to translate the string in a minimal time T from the
initial perturbed state (3) to the final state
That is, to extinguish the initial perturbations in a time T . Conditions (3) are equivalent to equating of the next
functional to zero.</p>
      <p>u(T, x) = 0;</p>
      <p>ut(T, x) = 0.</p>
      <p>J (T ) = ∫ [u2(T, x) + ut2(T, x)]dx = 0.</p>
      <p>To cancel the vibrations, we use a stationary pointwise actuator placed at the point x0.Then the function
f (t, x) will be sought in the form:
f (t, x) = W (t)δ(x
x0),
where x0 is the point of application of the actuator, δ is the Dirac delta function, W (t) is the control function.
(4)
(5)
(6)
(7)
(8)
(9)
(10)
(11)</p>
      <p>The initial conditions will take the form,
Consider the equation (1). We introduce auxiliary function υ(t, x) such that the equation (1) can be represented
as two first-order equations</p>
      <p>The system (7) can be written in the form of a characteristic system of ordinary differential equations
0</p>
      <p>l
{ut =
υx</p>
      <p>2V0ux
υt = (V02</p>
      <p>c2)ux + g(t, x).
g(t, x) =</p>
      <p>f (t, x) dx.
x
∫
0
l
We introduce in the calculated domain a grid formed by the lines xm = mh, h = ; m = 0, 1, ..., M , tn = nτ ;
M
n = 0, 1, ..., N , T = τ N , where h and τ respectively the grid steps. We will assume that c, V0 are integers and
τ = h (then the characteristics of different families will pass through the nodal points of the grid). In grid nodes
we introduce grid functions</p>
      <p>n
fumgm 2 0; M ,
n 2 0; N</p>
      <p>n
fυmgm 2 0; M .</p>
      <p>n 2 0; N
Let A 6 m 6 M + B, where A = V0 + c, B = V0
calculated area,</p>
      <p>c. Consider the three nodes in Figure 1, that lie within the
We approximate the equation (1) with the second order along the characteristic, connected the points ( n )
m</p>
      <p>A
and (n m+ 1), by the finite-difference scheme
And along the characteristic, connected the points (n + 1)
m
and</p>
      <p>(m n B), by a finite-difference scheme
(Au + υ)nm+1</p>
      <p>(Au + υ)nm A = τ gmn+1 +2 gmn A ,
(Bu + υ)nm+1</p>
      <p>(Bu + υ)nm B = τ gmn+1 +2 gmn B .</p>
      <p>From these equations, the values unm+1 and υmn+1 are easily found.</p>
      <p>Consider the case m &lt; A.</p>
      <p>In this case, for calculations, we find the values of upn υpn using quadratic interpolation at the three nearest
points. Taking into account, that from (2) u0n+r = 0, we find</p>
      <p>Now, finding υ0n+r, we can compose and solve the following system of equations
Similarly solved case m &gt; M + B.</p>
      <p>
(Au + υ)nm+1
(Bu + υ)nm+1
(Au + υ)0n+r = τ gmn+1 + g0n+r</p>
      <p>1 r 2
(Bu + υ)nm B = τ gmn+1 + gmn B</p>
      <p>2
2.2</p>
    </sec>
    <sec id="sec-2">
      <title>Method of Minimization</title>
      <p>To solve the problem of damping the string, we seek a control function W(t) for minimizing the integral (5) using
the Hook-Jeeves method.</p>
      <p>To do this, we approximate the function W (t) with a piecewise constant function: 8t 2 [ti, ti+1], W (t) = wi,
wi = const, i = 0, 1, ..., N 1.</p>
      <p>Then the integral (5) will be a function of the variables w0, w1, ..., wN 1</p>
      <p>J (T ) = J (w0, w1, ..., wN 1)</p>
      <p>The optimal value w0, w1, ..., wN 1 minimizing the integral with a given accuracy ε and being the desired
solution of the problem, will be found by the Hook-Jeeves method. To calculate the integral numerically, we use
the following approximation</p>
      <p>J (T ) =</p>
      <p>M 1
∑ [(uNm)2 + ( uNm
m=1
uNm 1
τ
)2]
(12)</p>
      <p>The condition for cancellating in the examples below is J (T ) 6 ε.
3
3.1</p>
      <p>Examples of Calculations</p>
    </sec>
    <sec id="sec-3">
      <title>Example 1</title>
      <p>As an example, let us consider the problem with the following parameter values: V0 = 1, c = 2, l = 1, M = 10.
The initial perturbations are given by the relations φ(x) = sin(πx), ψ(x) = 0.
As another example of calculations, consider the problem with the following parameter values: V0 = 1, c = 2, l =
1, M = 10. The initial perturbations are given by the relations φ(x) = x(1 x), ψ(x) = 0.</p>
      <p>Figure 6 shows the graph of the function u(t, x) without a control action, when f (t, x) = 0. It can be seen
that the string makes infinite fluctuations.</p>
      <p>Let us see problem of demping this oscilation. The initial parameters is x0 = 0.5 , ε = 0.005, T = 1.3 and
N = 13.</p>
    </sec>
    <sec id="sec-4">
      <title>Acknowledgements</title>
      <p>This work was supported by Russian Science Foundation, Project 17-19-01247.</p>
    </sec>
  </body>
  <back>
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            ,
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          </string-name>
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            <surname>A. G.</surname>
          </string-name>
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          ).
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</article>