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Thanks

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One gear is arranged so that it only experiences rotational motion ... Next a rod of length l is attached to the edge of the moving gear. ... Orbit Hunting ... – PowerPoint PPT presentation

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Title: Thanks


1
Thanks
  • I would like to thank all of those who helped me
    through my time as a Masters Student. Their help
    in classes and in projects was greatly
    appreciated.
  • I feel that it is necessary to thank my
    supervisor Dr. Randy Kobes, who has helped me not
    only in Thesis projects, but in my decisions
    through my career and for the future. I am not
    sure where I would be without his support.
  • This show has been brought to you by the letters
  • N - S - E - R - C

2
Chaotic Analysis
  • Periodic Orbit Theory

Andrew J Penner Randy Kobes Slaven Peles
3
The System
  • Our system was a simple setup of 2 gears, and a
    rod
  • This system was set vertically so the effects of
    gravity are ignored.
  • One gear is arranged so that it only experiences
    rotational motion
  • The second gear is stuck to the surface of the
    first gear, and may move around in a circle
    around the first gear.
  • Next a rod of length l is attached to the edge of
    the moving gear. The rod is capable of 360 degree
    motion.
  • The point of interest in this system in the
    coordinates at the free tip of the rod. The first
    simplifying assumption is that the angular
    frequency of the moving gear is constant at

4
The Gear and Rod Assembly
5
Mechanics
  • What we have from the previous slide is the
    coordinates defined as
  • x(R'R)cos(f')-Rcos(f'-f)lcos(q)
  • y(R'R)sin(f')-Rsin(f'-f)lsin(q)
  • If we consider R'f' Rf,. And take the gear
    ratio to be r R/R'
  • this results in a Lagrangian equation of

6
Equations of Motion
  • From the Lagrangian, and our first simplifying
    assumption we can easily determine the equation
    of motion for the rod angle,
  • To make the system more realistic we consider a
    frictional term
  • Then insert it into our equation of motion to get
  • Now we have an non-autonomous system, to be of
    more value to our calculations we may consider
    the autonomous version by introducing a
    dimensionless time variable twot. Since our
    assumption has been that the driving frequency is
    constant the phase space for the system consists
    of 3 dimensions ( ) and since f is time
    dependent we expect it to be smooth.
  • To simplify matters even more, we may reduce the
    problem to 2 degrees of freedom by using
    Poincare's theorem over the smooth variable f,
    which states that any system may be represented
    in full detail if one only takes a stroboscopic
    view of the attractor. This was done by using a
    common PDE solver and only recording discrete
    evolution steps.

7
Chaos
  • There are a few major considerations for a system
    to be considered chaotic. These were developed by
    Devaney
  • 1. The trajectory must be transitive
  • 2. The topology must be dense
  • 3. The trajectory must be non-repeating
  • Not all three conditions are necessary, but if
    all three are met you can be assured that chaos
    exists.

8
Stroboscopic Effect
  • What we see is a great simplification from the
    projection of the attractor onto the 2D plane.

9
Bifurcation
  • An important feature of a chaotic system is the
    dependence that each of the paramters of the
    system must have wrt each other. This dependence
    may be best seen in a bifurcation diagram.
    Furthermore, it is in one of these diagrams that
    the chaos in the system may be located, for
    example consider the logistic diagram. Insert a
    few bifurcation diagram pictures.
  • In similar diagrams produced by our system, we
    found several chaotic regimes existsed, the 2 of
    greatest interest was Q0.76, a 1.028, r
    1.088
  • and Q 1.2577, a 1.17731, r 1.088.

10
Bifurcation Diagram
11
Focused Bifurcation Diagrams
12
Lyapunov Index
  • With the chaotic regime located, a natural next
    question to ask is the degree of chaos given the
    specific parameters. This is measured by the
    Lyapunov index, an exponential value that
    determines how fast a system moves from a
    predictable state to an unpredictable state.
    Traditionally this is measured with averages of a
    pair of trajectories as they evolve, and separate.

13
Lyapunov Exponent
  • The Lyapunov index measures the rate of
    divergence between a trajectory with 2 different
    initial conditions

14
Winding Number
  • The winding (rotation) number is used to
    determine the convergence of a closed dynamical
    system. Essentially we are observing a path of a
    trajectory through coordinate space. This value
    is rational if the system contains periodic
    paths. For a chaotic system one expects an
    irrational winding number, signifying that the
    orbits on a manifold are not periodic, thus never
    repeating. Like with the case of the Lyapunov
    exponent, the winding number is traditionally
    measured with an average over the system.

15
Winding Number R
  • The Winding Number is a method of tracking a
    trajectory around phase space.
  • The black line in the above picture displays a
    winding number of 2/5, since it is rational the
    trajectory is nonchaotic
  • The winding number is defined as the asymptotic
    limit over the entire trajectory

16
Symbolic Dynamics
  • Symbolic dynamics started by a fellow named
    Hadamard. He was using this method to solve for
    allowed trajectories on spaces of negative
    curvature. Since then there have been several
    applications of this method to physical dynamical
    systems. The idea behind symbolic dynamics is
    that one can trace the path a trajectory takes in
    phase space, by the regions that it passes
    through. This has definite advantages to tracing
    the numerical coordinates of a trajectory
    especially in chaotic dynamics where a true
    representation of a trajectory would require
    infinite precision. The difficult part of this
    method lies in the determination of the
    partitions in phase space.

17
Symbolic Dynamics
The symbol planes for Q 0.76 and Q 1.2577 for
periods up to period 15. The x-axis represents
forward iterations, the y-axis represents
backward iterations.
18
Partitioning
  • The breaking of phase space can be made simple by
    the construction of a return map, a map that
    takes a coordinate of phase space and plots it
    against the same coordinate in the next
    evolutionary step. Using this map one could use
    the locat maxima and minima as partitions points,
    howver this method does not work all that well
    for systems with 2 dimensional tendencies, since
    these attractors tend to be double sheeted. If
    one were to use the local maxima and minima
    method, one may end up using more symbols than
    necessary to describe the system. This leads to
    difficulties in later calculations. The method of
    choice was the homoclinic points, where one maps
    the forward iterative map onto the attractor, and
    marks the points of tangency. This method ensures
    a minimal number of symbols used for a system.

19
Partitioning
  • The homoclinic partitioning points as seen on
    both the Poincare section, and the first return
    map

20
Symbols
  • When calculating the symbolic dynamics of
    possible paths through symbol space the user only
    needs to produce a list of all possible
    permutations and combinations of the symbols
    used, to any period desired. Of course if we
    could leave the list like this, we would
    essentiually be saying that the trajectory of the
    system could go anywhere anytime. Physically we
    expect that this should not be the case, and we
    must consider a set of symbolic limits or
    rules that restrict the orbit in some way.
    These are referred to as fundamental forbidden
    zones. These are regions determined by a return
    map, that may never be entered by any part of a
    trajectory. These are determined in a 1D case by
    a forward iteration on the return map from a
    homoclinic point. For a 2D map one needs to also
    consider the possible reverse iterations (how did
    the trajectory get here points) that form the
    secondary restrictions to a symbolic dynamic
    orbit. Since these orbits are periodic one expect
    repetition in the orbit, and we find that we have
    to test all cyclic permutations of an orbit to
    determine its viability.

21
Symbolic Mathematics
  • To determine the rules for allowable orbits one
    must associate a measure to our symbolic system.
  • We associate a number in the unit interval to the
    forward and backward sequences. What is common,
    is to associate a sign change depending on the
    value of the symbolic orbit, in our case we chose
    to associate a sign change whenever the symbol N
    appeared in the sequence. The next requirement
    was to create a numerical value for the forward
    sequence.
  • Where mi 0,1,2 for si L,R,N if the product of
    the e is one up to that symbol, otherwise mi
    2,1,0 for si L,R,N

22
Symbolic Mathematics
  • We perform a similar procedure for the backward
    sequence.
  • The value of the symbol is determined by
  • Where ni 0,1,2 for si R,N,L if the product of
    the e is one up to that symbol, otherwise ni
    2,1,0 for si R,N,L

23
Ordering
  • Now the symbolic measure has been constructed we
    may consider the natural ordering of a symbolic
    set
  • This ordering allows us to talk about the winding
    number as a feature of our chaotic system.
  • Insert ordering picture

24
Orbit Hunting
  • So far the symbolic dynamics has been defines,
    and we have our list of possible orbits. For
    these to be of any futher use, we require the
    ability to actually locate the numerical values
    at least approximately, of these trajectories in
    phase space. Doing this required a few
    techniques, the most important was the use of the
    existance of pseudocycles. Since each pseudocycle
    will always shadow a prime cycle one could simply
    use the smaller orbital positions as guesses for
    larger prime cycles. This had a very high success
    rate. A second method would break up already
    found orbits, and use the peices to make up the
    guesses for larger cycles. This was used as a
    last resort since it is a time consuming process.
    A problem arose with the exponentially increasing
    number of allowed orbits. Methods of combination
    of old orbits became tedious and did not always
    return proper results. This was especially true
    of orbits with very large instability. At this
    point the search method was set up to test all
    possible combinations of points along the
    attractor. Automated methods were much easier,
    but were time consuming, fortunately machines
    like to run night and day for several months.
    Ultimately we came to the conclusion that we
    needed only the more stable orbits, and reduced
    our search a little further. Our search for
    orbits terminated at period 30.

25
Orbit Hunting
  • For short orbits, the first return map was
    essential for finding the allowed orbits, the
    left is the first return map, the right is the
    second return map both for Q 0.76

26
Larger Orbit Hunting
  • RNNRRL ? RNN-RRL ? RNN, RRL
  • ? RNNR-RL ? RRNN, RL
  • RRRNLL ? RRRN-LL ? RRRN, NRLL

27
Shadowing
  • The symbolic dynamics described so far involves
    what is referred to as prime orbits or prime
    cycles. Another set of orbits are referred to as
    pseudo-orbits, or pseudo cycles. These are a set
    of orbits made by joining 2 or more prime cycles.
    Physically they look very similar, and
    mathimatically they are also very similar. A
    complete symbolic dynamic description requires
    both sets of values. For example consider the
    period 4 orbit RNRL, and the 2 period 2 orbits,
    RN and RL. One could combine the 2 period 2
    orbits to make RN-RL a pseudocycle whith similar
    properties as the prime cycle RNRL.

28
Shadowing
For kth order shadowing orbits Lp L1 L2
L3Lk np n1 n2 n3 nk Tp T1 T2 T3
Tk Ap A1 A2 A3 Ak Where A is
any observable that may be extracted from the
system
29
Dynamical Averaging
  • Now we fix our dynamical system by adding in some
    statistical mechanics. Because nothing really
    makes something sound complicated like
    statistical mechanics. We have around 10000
    orbits, each are periodic, and some slightly more
    stable than others. But the question is What do
    we want with them, or how do they relate to
    chaotic dynamics? Well, in the next several
    slides of very complicated code, we will discuss
    line by line how each of these orbits contributed
    to the analysis of the chaos in the system and
    four alternate commands that could have been used.

30
Eigenvalues
  • The most important peice of information that is
    drawn from the periodic orbits is the stability
    eigenvalue. Each of these orbits contained a
    point in phase space which was used to solve the
    Jacobian matrix. The Jacobian matrix for each
    point in the trajectory was then multiplied, and
    the eigenvalues of the resulting matrix were
    determined. One expects the eigenvalues to sum to
    a negative value, due to the divergence of the
    system. By Haken's theorem, we expect that one of
    the eigenvalues will be 1. There in we obtain two
    eigenvalues, one greater than zero, and one less
    than zero. The eigenvalue that is less than zero
    corresponds to a stable contractive system, the
    eigenvalue that is greater than zero corresponds
    to an expanding unstable system. The positive
    eigenvalue is the eigenvalue of interest. These
    play a very important role in the dynamical
    averaging of a system.

31
Eigenvalues
  • Nonlinear flow equations are difficult to
    evaluate analytically and thus we use
    approximations to linearize the flow

When calculating the eigenvalues one just
multiplies the matrix J
Now find the eigenvalues Li of Ji
32
Dynamical Averaging
  • Following the averaging formula
  • We are after a space average of the observable
    a(xt)
  • Using geometric arguments over phase space we
    find that for infinitesimal strip of phase space
    Mi is approximately equal to the unstable
    eigenvalue Li of the orbit occupying that space.
    This allows the spatial average to be reduced to
    a discrete sum over all the orbits, further
    considering that we want a full averaged system,
    we also expect to average over time,
  • which in the case of periodic orbits is a sum
    over each element in the orbit. Ultimately after
    considering all the averages we have a double
    sum

33
Three Observables
  • We have 3 observables, the escape rate, the
    Lyapunov exponent, and the winding number
  • When considering these values and the periodic
    orbit theory, all we have to do is replace Ap
    with the following values
  • Where Rp is the winding ratio of the pth periodic
    orbit

34
Escape Rate g
35
Winding Number R
36
Lyapunov Exponent
37
Summary of Results
  • We found the expectation that the escape rate is
    zero was met by both systems
  • The Winding Number met the brute force value
    within decimal places
  • The Lyapunov exponent also met the brute force
    value within decimal places

38
Future Possibilities
  • Better analysis may be performed or better
    results by use of smoothing
  • Applications of this research are open to any
    chaotic system that has one or two dimensions
  • Researching symbolic dynamics for higher
    dimensional systems is the only restriction, the
    methods for dynamical averaging are open to
    higher dimension?

39
References
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