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June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 11
Analysis of Aircraft Nonlinear Dynamics
Based on Parametric Continuation and
Phase Portrait Investigation
Dr MikhailDr Mikhail GomanGoman and Dr Andrewand Dr Andrew KhramtsovskyKhramtsovsky
DeDe MontfortMontfort University, Leicester, the UKUniversity, Leicester, the UK
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 22
ContentsContents
nn Goals and tools of applied bifurcation analysisGoals and tools of applied bifurcation analysis
nn Permanent retention of computed data in a databasePermanent retention of computed data in a database
structure: new algorithms, new possibilitiesstructure: new algorithms, new possibilities
nn Phase portrait analysisPhase portrait analysis
nn ExamplesExamples
nn ConclusionsConclusions
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 33
Typical goals of the BifurcationTypical goals of the Bifurcation
Analysis (BA)Analysis (BA)
nn In the parameter space:In the parameter space:
–– to find boundaries between the regions withto find boundaries between the regions with
different types of the nonlinear systemdifferent types of the nonlinear system’’s dynamicss dynamics
nn In the state space:In the state space:
–– To find out all the steadyTo find out all the steady--state solutionsstate solutions
(equilibrium, periodic, strange attractors) and to(equilibrium, periodic, strange attractors) and to
study their evolution with respect to thestudy their evolution with respect to the
parameters,parameters,
–– To understand each type of the nonlinear systemTo understand each type of the nonlinear system’’ss
dynamicsdynamics
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 44
Aircraft Rigid Body DynamicsAircraft Rigid Body Dynamics
Equations of Motion
State Variables
Control Variables
w
w
w
ww
d
d
d
d
d
d
d
d
t
t
t
t
I + Ix = Ma+Mc
V
m + V = F+T + Gx( ) a
R
=
=
C( )
)
VQ
Q
Q E(
Q q f y
w
a
a
b
b
b
d d d d d d
h h z
R =
=
=
(X Y Z )g g g
(
(
)
)
V
= p q r
T
T
T
T
T
V
V
V
cos cos
cos
sin
sin
e er l
l l
=
=
(
(
)
)
a r c...
T T Tr r
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 55
Numerical MethodsNumerical Methods
for Qualitative Analysisfor Qualitative Analysis
nn Continuation algorithm:Continuation algorithm:
–– branching and limit pointsbranching and limit points
processing;processing;
–– systematic search for all solutionssystematic search for all solutions
of nonlinear system at fixedof nonlinear system at fixed
parameters;parameters;
–– bifurcation points identificationbifurcation points identification
and collectionand collection
nn Regions of attraction:Regions of attraction:
–– reconstruction of stability regionreconstruction of stability region
boundary;boundary;
–– computation of twocomputation of two--dimensionaldimensional
cross sectionscross sections
nn Numerical simulation:Numerical simulation:
–– perturbations in particularperturbations in particular
manifolds of trajectories;manifolds of trajectories;
detF = 0
det = 0F
x
s
x
c
limit point
branching point
parameter variation
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 66
SteadySteady--state solutionsstate solutions
and their evolutionand their evolution
nn Computationally intensive, but relativelyComputationally intensive, but relatively
straightforward taskstraightforward task
nn Main tool is the continuation technique:Main tool is the continuation technique:
–– Bifurcation points and alternative branches areBifurcation points and alternative branches are
determineddetermined ““on the flyon the fly””
–– All the data (the branches, stability data,All the data (the branches, stability data,
bifurcation and other special points) arebifurcation and other special points) are
recorded in the permanent databaserecorded in the permanent database
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 77
1D bifurcations diagrams: equilibriums1D bifurcations diagrams: equilibriums
(computed using(computed using KritKrit package)package)
Legend:Legend:
nn StableStable
nn OscillatoryOscillatory
unstableunstable
nn AperiodicallyAperiodically
unstableunstable
nn UnstableUnstable
(other types)(other types)
BranchingBranching
pointspoints
TestTest ““KubichekKubichek--88””
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 88
1D bifurcations diagrams:1D bifurcations diagrams:
periodic solutionsperiodic solutions
nn For the closedFor the closed
orbits the minimumorbits the minimum
and maximumand maximum
values of X(1) statevalues of X(1) state
vector componentvector component
are plottedare plotted vsvs thethe
parameter valueparameter value
nn Both timeBoth time--advanceadvance
andand PoincarePoincare
mappings weremappings were
used during theused during the
computationscomputations
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 99
1D bifurcations diagrams: complex1D bifurcations diagrams: complex
attractors and jumpsattractors and jumps
nn Continuation of the complexContinuation of the complex
attractors:attractors:
–– fixed increments of the parameterfixed increments of the parameter
–– IntegrationIntegration
nn Jumps: Analysis of the systemJumps: Analysis of the system’’ss
behavior near the bifurcation pointsbehavior near the bifurcation points
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1010
Example: Lorenz modelExample: Lorenz model
andand rr -- varvar
Parameter values are:Parameter values are:
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1111
Equilibrium and periodic solutionsEquilibrium and periodic solutions
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1212
Lorenz strange attractorLorenz strange attractor
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1313
Continuation of the complex attractorContinuation of the complex attractor
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1414
Stability of the complex attractor:Stability of the complex attractor:
LyapunovLyapunov indicesindices
nn One index shouldOne index should
always be equalalways be equal
to zeroto zero
nn Stable complexStable complex
attractor has oneattractor has one
positivepositive LyapunovLyapunov
indexindex
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1515
Evolution diagram:Evolution diagram:
useful tool for recovery studiesuseful tool for recovery studies
nn The diagramThe diagram
shows how toshows how to
enter into andenter into and
to recoverto recover
from certainfrom certain
stable regimestable regime
nn During thisDuring this
analysis newanalysis new
solutionssolutions
could becould be
foundfound
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1616
2D bifurcations diagrams2D bifurcations diagrams
(computed using(computed using KritKrit package)package)
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1717
2D bifurcations diagrams2D bifurcations diagrams
(computed using(computed using KritKrit package)package)
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1818
Permanent database gives rise to aPermanent database gives rise to a
new classes of algorithmsnew classes of algorithms
nn Permanent memory makes the algorithms trulyPermanent memory makes the algorithms truly
intelligent: they can capitalize on the previousintelligent: they can capitalize on the previous
resultsresults
nn Some possibilities:Some possibilities:
–– Faster search for the steadyFaster search for the steady--state solutions by usingstate solutions by using
known solutions as initial guesses,known solutions as initial guesses,
–– Possibility to stop simulation if stable steadyPossibility to stop simulation if stable steady--statestate
solution is approached,solution is approached,
–– Possibility to identify statePossibility to identify state--space structures, or tospace structures, or to
check completeness of the bifurcation diagrams,check completeness of the bifurcation diagrams,
–– And many moreAnd many more ……
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1919
1D Permanent database contains:1D Permanent database contains:
nn Branches of the steadyBranches of the steady--state solutionsstate solutions
including stability data and trajectories ofincluding stability data and trajectories of
periodic solutions and strange attractors,periodic solutions and strange attractors,
nn Starting points, bifurcation points, error pointsStarting points, bifurcation points, error points
etc.etc.
nn Branching information computed for bifurcationBranching information computed for bifurcation
pointspoints
nn Data on relationships between bifurcationData on relationships between bifurcation
points and branchespoints and branches
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2020
Database Structure for Nonlinear AutonomousDatabase Structure for Nonlinear Autonomous
System: UML descriptionSystem: UML description
Class diagram for the autonomous nonlinear dynamical systemClass diagram for the autonomous nonlinear dynamical system
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2121
Example: completeness checkExample: completeness check
((““AdvisorAdvisor”” module)module)
nn Test KubicheckTest Kubicheck--88
nn At the end theAt the end the
database containsdatabase contains
dozens of specialdozens of special
points and continuationpoints and continuation
trajectories.trajectories.
nn ““ManualManual”” analysis isanalysis is
difficultdifficult
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2222
nn inconsistenciesinconsistencies
in the databasein the database
are identifiedare identified
nn inconsistenciesinconsistencies
can be visualizedcan be visualized
nn recoveryrecovery
probability isprobability is
evaluatedevaluated
nn autoauto--repairrepair
featurefeature
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2323
Phase portrait analysisPhase portrait analysis
nn SystemSystem’’s dynamics is studied at a parameters dynamics is studied at a parameter
valuesvalues ““typicaltypical”” for a certain type of it.for a certain type of it.
nn The following is computed:The following is computed:
a.a. SteadySteady--state solutions and their stability (may bestate solutions and their stability (may be
extracted from the permanent memory),extracted from the permanent memory),
b.b. Special trajectories (incoming to or outgoing from aSpecial trajectories (incoming to or outgoing from a
steadysteady--state solution along the eigenvectors)state solution along the eigenvectors)
c.c. SimulationsSimulations
d.d. CrossCross--sections of the regions of attraction of stablesections of the regions of attraction of stable
steadysteady--state solutionsstate solutions
b.b.--d. may result in finding new steadyd. may result in finding new steady--state solutionsstate solutions
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2424
Phase Portrait GUI and databasePhase Portrait GUI and database
KubicheckKubicheck--88
problemproblem
nn The databaseThe database
contains multiplecontains multiple
equilibriumequilibrium
solutions andsolutions and
specialspecial
trajectoriestrajectories
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2525
Partial automationPartial automation
of the phase portrait analysisof the phase portrait analysis
Phase Portrait GUI (KRIT package):Phase Portrait GUI (KRIT package):
nn SteadySteady--state solutions and stability data arestate solutions and stability data are
extracted from 1D Permanent databaseextracted from 1D Permanent database
nn Special trajectories are computedSpecial trajectories are computed
nn Optionally points belonging to a separating surfaceOptionally points belonging to a separating surface
between two stable attractors are computed. Thisbetween two stable attractors are computed. This
often leads to the finding of unstable periodicoften leads to the finding of unstable periodic
solutions.solutions.
nn UserUser--controlled simulation and computation of thecontrolled simulation and computation of the
crosscross--sections of asymptotic stability regionssections of asymptotic stability regions
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2626
FF--18, 818, 8thth
order: Computation of ASRorder: Computation of ASR
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2727
FF--18 with FCS: Computation of ASR18 with FCS: Computation of ASR
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2828
ConclusionsConclusions
nn Continuation and mapping technique areContinuation and mapping technique are
powerful tools. Comprehensive database of thepowerful tools. Comprehensive database of the
results obtained multiplies their power andresults obtained multiplies their power and
allows to construct new algorithms.allows to construct new algorithms.
nn GUIs make continuation and phase portraitGUIs make continuation and phase portrait
computations flexible. More automation iscomputations flexible. More automation is
necessary.necessary.
nn Advances in the computing of regions ofAdvances in the computing of regions of
attraction are highly desirable.attraction are highly desirable.
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2929
AcknowledgementsAcknowledgements
nn This research was funded byThis research was funded by
QinetiQQinetiQ/DERA (Bedford, the UK)/DERA (Bedford, the UK)
June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 3030
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M.Goman, A.Khramtsovsky (2006) - Analysis of Aircraft Nonlinear Dynamics Based on Parametric Continuation and Phase Portrait Investigation

  • 1. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 11 Analysis of Aircraft Nonlinear Dynamics Based on Parametric Continuation and Phase Portrait Investigation Dr MikhailDr Mikhail GomanGoman and Dr Andrewand Dr Andrew KhramtsovskyKhramtsovsky DeDe MontfortMontfort University, Leicester, the UKUniversity, Leicester, the UK
  • 2. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 22 ContentsContents nn Goals and tools of applied bifurcation analysisGoals and tools of applied bifurcation analysis nn Permanent retention of computed data in a databasePermanent retention of computed data in a database structure: new algorithms, new possibilitiesstructure: new algorithms, new possibilities nn Phase portrait analysisPhase portrait analysis nn ExamplesExamples nn ConclusionsConclusions
  • 3. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 33 Typical goals of the BifurcationTypical goals of the Bifurcation Analysis (BA)Analysis (BA) nn In the parameter space:In the parameter space: –– to find boundaries between the regions withto find boundaries between the regions with different types of the nonlinear systemdifferent types of the nonlinear system’’s dynamicss dynamics nn In the state space:In the state space: –– To find out all the steadyTo find out all the steady--state solutionsstate solutions (equilibrium, periodic, strange attractors) and to(equilibrium, periodic, strange attractors) and to study their evolution with respect to thestudy their evolution with respect to the parameters,parameters, –– To understand each type of the nonlinear systemTo understand each type of the nonlinear system’’ss dynamicsdynamics
  • 4. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 44 Aircraft Rigid Body DynamicsAircraft Rigid Body Dynamics Equations of Motion State Variables Control Variables w w w ww d d d d d d d d t t t t I + Ix = Ma+Mc V m + V = F+T + Gx( ) a R = = C( ) ) VQ Q Q E( Q q f y w a a b b b d d d d d d h h z R = = = (X Y Z )g g g ( ( ) ) V = p q r T T T T T V V V cos cos cos sin sin e er l l l = = ( ( ) ) a r c... T T Tr r
  • 5. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 55 Numerical MethodsNumerical Methods for Qualitative Analysisfor Qualitative Analysis nn Continuation algorithm:Continuation algorithm: –– branching and limit pointsbranching and limit points processing;processing; –– systematic search for all solutionssystematic search for all solutions of nonlinear system at fixedof nonlinear system at fixed parameters;parameters; –– bifurcation points identificationbifurcation points identification and collectionand collection nn Regions of attraction:Regions of attraction: –– reconstruction of stability regionreconstruction of stability region boundary;boundary; –– computation of twocomputation of two--dimensionaldimensional cross sectionscross sections nn Numerical simulation:Numerical simulation: –– perturbations in particularperturbations in particular manifolds of trajectories;manifolds of trajectories; detF = 0 det = 0F x s x c limit point branching point parameter variation
  • 6. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 66 SteadySteady--state solutionsstate solutions and their evolutionand their evolution nn Computationally intensive, but relativelyComputationally intensive, but relatively straightforward taskstraightforward task nn Main tool is the continuation technique:Main tool is the continuation technique: –– Bifurcation points and alternative branches areBifurcation points and alternative branches are determineddetermined ““on the flyon the fly”” –– All the data (the branches, stability data,All the data (the branches, stability data, bifurcation and other special points) arebifurcation and other special points) are recorded in the permanent databaserecorded in the permanent database
  • 7. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 77 1D bifurcations diagrams: equilibriums1D bifurcations diagrams: equilibriums (computed using(computed using KritKrit package)package) Legend:Legend: nn StableStable nn OscillatoryOscillatory unstableunstable nn AperiodicallyAperiodically unstableunstable nn UnstableUnstable (other types)(other types) BranchingBranching pointspoints TestTest ““KubichekKubichek--88””
  • 8. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 88 1D bifurcations diagrams:1D bifurcations diagrams: periodic solutionsperiodic solutions nn For the closedFor the closed orbits the minimumorbits the minimum and maximumand maximum values of X(1) statevalues of X(1) state vector componentvector component are plottedare plotted vsvs thethe parameter valueparameter value nn Both timeBoth time--advanceadvance andand PoincarePoincare mappings weremappings were used during theused during the computationscomputations
  • 9. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 99 1D bifurcations diagrams: complex1D bifurcations diagrams: complex attractors and jumpsattractors and jumps nn Continuation of the complexContinuation of the complex attractors:attractors: –– fixed increments of the parameterfixed increments of the parameter –– IntegrationIntegration nn Jumps: Analysis of the systemJumps: Analysis of the system’’ss behavior near the bifurcation pointsbehavior near the bifurcation points
  • 10. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1010 Example: Lorenz modelExample: Lorenz model andand rr -- varvar Parameter values are:Parameter values are:
  • 11. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1111 Equilibrium and periodic solutionsEquilibrium and periodic solutions
  • 12. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1212 Lorenz strange attractorLorenz strange attractor
  • 13. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1313 Continuation of the complex attractorContinuation of the complex attractor
  • 14. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1414 Stability of the complex attractor:Stability of the complex attractor: LyapunovLyapunov indicesindices nn One index shouldOne index should always be equalalways be equal to zeroto zero nn Stable complexStable complex attractor has oneattractor has one positivepositive LyapunovLyapunov indexindex
  • 15. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1515 Evolution diagram:Evolution diagram: useful tool for recovery studiesuseful tool for recovery studies nn The diagramThe diagram shows how toshows how to enter into andenter into and to recoverto recover from certainfrom certain stable regimestable regime nn During thisDuring this analysis newanalysis new solutionssolutions could becould be foundfound
  • 16. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1616 2D bifurcations diagrams2D bifurcations diagrams (computed using(computed using KritKrit package)package)
  • 17. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1717 2D bifurcations diagrams2D bifurcations diagrams (computed using(computed using KritKrit package)package)
  • 18. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1818 Permanent database gives rise to aPermanent database gives rise to a new classes of algorithmsnew classes of algorithms nn Permanent memory makes the algorithms trulyPermanent memory makes the algorithms truly intelligent: they can capitalize on the previousintelligent: they can capitalize on the previous resultsresults nn Some possibilities:Some possibilities: –– Faster search for the steadyFaster search for the steady--state solutions by usingstate solutions by using known solutions as initial guesses,known solutions as initial guesses, –– Possibility to stop simulation if stable steadyPossibility to stop simulation if stable steady--statestate solution is approached,solution is approached, –– Possibility to identify statePossibility to identify state--space structures, or tospace structures, or to check completeness of the bifurcation diagrams,check completeness of the bifurcation diagrams, –– And many moreAnd many more ……
  • 19. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 1919 1D Permanent database contains:1D Permanent database contains: nn Branches of the steadyBranches of the steady--state solutionsstate solutions including stability data and trajectories ofincluding stability data and trajectories of periodic solutions and strange attractors,periodic solutions and strange attractors, nn Starting points, bifurcation points, error pointsStarting points, bifurcation points, error points etc.etc. nn Branching information computed for bifurcationBranching information computed for bifurcation pointspoints nn Data on relationships between bifurcationData on relationships between bifurcation points and branchespoints and branches
  • 20. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2020 Database Structure for Nonlinear AutonomousDatabase Structure for Nonlinear Autonomous System: UML descriptionSystem: UML description Class diagram for the autonomous nonlinear dynamical systemClass diagram for the autonomous nonlinear dynamical system
  • 21. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2121 Example: completeness checkExample: completeness check ((““AdvisorAdvisor”” module)module) nn Test KubicheckTest Kubicheck--88 nn At the end theAt the end the database containsdatabase contains dozens of specialdozens of special points and continuationpoints and continuation trajectories.trajectories. nn ““ManualManual”” analysis isanalysis is difficultdifficult
  • 22. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2222 nn inconsistenciesinconsistencies in the databasein the database are identifiedare identified nn inconsistenciesinconsistencies can be visualizedcan be visualized nn recoveryrecovery probability isprobability is evaluatedevaluated nn autoauto--repairrepair featurefeature
  • 23. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2323 Phase portrait analysisPhase portrait analysis nn SystemSystem’’s dynamics is studied at a parameters dynamics is studied at a parameter valuesvalues ““typicaltypical”” for a certain type of it.for a certain type of it. nn The following is computed:The following is computed: a.a. SteadySteady--state solutions and their stability (may bestate solutions and their stability (may be extracted from the permanent memory),extracted from the permanent memory), b.b. Special trajectories (incoming to or outgoing from aSpecial trajectories (incoming to or outgoing from a steadysteady--state solution along the eigenvectors)state solution along the eigenvectors) c.c. SimulationsSimulations d.d. CrossCross--sections of the regions of attraction of stablesections of the regions of attraction of stable steadysteady--state solutionsstate solutions b.b.--d. may result in finding new steadyd. may result in finding new steady--state solutionsstate solutions
  • 24. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2424 Phase Portrait GUI and databasePhase Portrait GUI and database KubicheckKubicheck--88 problemproblem nn The databaseThe database contains multiplecontains multiple equilibriumequilibrium solutions andsolutions and specialspecial trajectoriestrajectories
  • 25. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2525 Partial automationPartial automation of the phase portrait analysisof the phase portrait analysis Phase Portrait GUI (KRIT package):Phase Portrait GUI (KRIT package): nn SteadySteady--state solutions and stability data arestate solutions and stability data are extracted from 1D Permanent databaseextracted from 1D Permanent database nn Special trajectories are computedSpecial trajectories are computed nn Optionally points belonging to a separating surfaceOptionally points belonging to a separating surface between two stable attractors are computed. Thisbetween two stable attractors are computed. This often leads to the finding of unstable periodicoften leads to the finding of unstable periodic solutions.solutions. nn UserUser--controlled simulation and computation of thecontrolled simulation and computation of the crosscross--sections of asymptotic stability regionssections of asymptotic stability regions
  • 26. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2626 FF--18, 818, 8thth order: Computation of ASRorder: Computation of ASR
  • 27. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2727 FF--18 with FCS: Computation of ASR18 with FCS: Computation of ASR
  • 28. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2828 ConclusionsConclusions nn Continuation and mapping technique areContinuation and mapping technique are powerful tools. Comprehensive database of thepowerful tools. Comprehensive database of the results obtained multiplies their power andresults obtained multiplies their power and allows to construct new algorithms.allows to construct new algorithms. nn GUIs make continuation and phase portraitGUIs make continuation and phase portrait computations flexible. More automation iscomputations flexible. More automation is necessary.necessary. nn Advances in the computing of regions ofAdvances in the computing of regions of attraction are highly desirable.attraction are highly desirable.
  • 29. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 2929 AcknowledgementsAcknowledgements nn This research was funded byThis research was funded by QinetiQQinetiQ/DERA (Bedford, the UK)/DERA (Bedford, the UK)
  • 30. June 21, 2006June 21, 2006 ICNPAAICNPAA--2006: Mathematical Problems in Engineering and Aerospace Science2006: Mathematical Problems in Engineering and Aerospace Sciencess 3030 Questions?