kang-min choi, graduate student, kaist, korea young-jong moon , graduate student, kaist, korea
DESCRIPTION
Algebraic Method for Eigenpair Derivatives of Damped System with Repeated Eigenvalues. Kang-Min Choi, Graduate Student, KAIST, Korea Young-Jong Moon , Graduate Student, KAIST, Korea Ji-Eun Jang , Graduate Student, KAIST, Korea - PowerPoint PPT PresentationTRANSCRIPT
Kang-Min Choi, Kang-Min Choi, Graduate Student, KAIST, Korea
Young-Jong MoonYoung-Jong Moon, Graduate Student, KAIST, Korea
Ji-Eun JangJi-Eun Jang, Graduate Student, KAIST, Korea
Woon-Hak Kim, Professor, Hankyong National University, Korea
In-Won LeeIn-Won Lee, Professor, KAIST, Korea
Algebraic Method for Eigenpair Derivatives of Damped System
with Repeated Eigenvalues
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OUTLINE
INTRODUCTION
PREVIOUS METHODS
PROPOSED METHOD
NUMERICAL EXAMPLE
CONCLUSIONS
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INTRODUCTION
determination of the sensitivity of dynamic response optimization of natural frequencies and mode shapes optimization of structures subject to natural frequencies
Applications of sensitivity analysis are
Typical structures have many repeated or nearly equaleigenvalues, due to structural symmetry.
The second- and higher order derivatives of eigenpairsare important to predict the eigenpairs, which relieson the matrix Taylor series expansion.
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 44
)( 2 0KCM
Problem Definition Problem Definition
(1)
K
C
M
Eigenvalue problem of damped system
shape) (moder eigenvecto :
frequency) (natural eigenvalue :
definite semi-positive matrix, Stiffness :
matrix Damping :
definite positive matrix, Mass :
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 55
,
,,, K ,C ,M
K C, M,
,, ,
Given:
Find:
* represents the derivative of with respect design parameter α (length, area, moment of inertia, etc.)
,)( )(
Objective of this study: Objective of this study:
,, ,
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PREVIOUS STUDIES
Damped system with distinct eigenvalues K. M. Choi, H. K. Jo, J. H. Lee and I. W. Lee, “Sensitivity
Analysis of Non-conservative Eigensystems,” Journal of Sound and Vibration, 2001. (Accepted)
jjj
jj
j
j
jjjj
jjjj
)CM2(5.0
)KCM(
M)CM2(
)CM2(KCM
,,
,,,
,
,2
T
T
TT
- The coefficient matrix is symmetric and non-singular.
- Eigenpair derivatives are obtained simultaneously.
- The algorithm is simple and guarantees stability.
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Undamped system with repeated eigenvalues R. L. Dailey, “Eigenvector Derivatives with Repeated
Eigenvalues,” AIAA Journal, Vol. 27, pp.486-491, 1989.
- Introduction of Adjacent eigenvector
- Calculation derivatives of eigenvectors by the sum of homogenous solutions and particular solutions using Nelson’s algorithm
- Complicated algorithm and high time consumption
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 88
Second order derivatives of Undamped systemwith distinct eigenvalues
M. I. Friswell, “Calculation of Second and Higher Eigenvector Derivatives”, Journal of Guidance, Control and Dynamics, Vol. 18, pp.919-921, 1995.
j,jjjj,jjj
jjjjjj
)MMK()MMK(
)MMMK(
,,,,,,
,,,,,,,
TT
T
(3)
jjjj cv,
where j,jj,jjjj ,,,T )MK()MK(M5.0c
(4)
- Second eigenvector derivatives extended by Nelson’s algorithm
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 99
PROPOSED METHOD
First-order eigenpair derivatives of damped systemwith repeated eigenvalues
Second-order eigenpair derivatives of damped systemwith repeated eigenvalues
Numerical stability of the proposed method
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First-order eigenpair derivatives of damped systemwith repeated eigenvalues
Basic Equations
• Eigenvalue problem
(5)
(6)
0KCM 2 mmmmm
mmmm I)CM2(T
• Orthonormalization condition
mm
m
seigenvalue repeated ofy mutiplicit ofnumber the:
rseigenvecto ofmatrix the
( seigenvalue ofmatrix the
:
)I: mmm
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TX mm
mITTT
(7)
where T is an orthogonal transformation matrixand its order m
(8)
Adjacent eigenvectors
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• Rearranging eq.(5) and eq.(6) using adjacent eigenvectors
0KXXCXM 2 mmmmm
mmmm IX)CM2(XT
(9)
(10)
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• Differentiating eq.(9) w.r.t. design parameter α
mmm
mmmmmm
X)KCM(
X)CM2(X)KCM(
,,,2
,,2
(11)
• Pre-multiplying at each side of eq.(11) by and
substituting
Tm
TX mm
,TDT m
mmmm )KCM(D ,,,2T
(12)
where
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 1414
• Differentiating eq.(9) w.r.t. design parameter α
(13)
(14)
mmm
mmmm
X)KCM(
X)CM2()KCM(
,,,2
2
,Xm ,m
• Differentiating eq.(10) w.r.t. design parameter α
mmm
mmmm
X)CM2(X5.0
XMX )CM2(X
,,T
TT
,Xm ,m
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 1515
mmm
mmm
m
m
mmmm
mmmm
X)CM2(X5.0
X)KCM(
X
XMX)CM2(X
X)CM2(KCM
,,T
,,,2
,
,
TT
2
(15)
- It maintains N-space without use of state space equation.
- Eigenpair derivatives are obtained simultaneously.
- It requires only corresponding eigenpair information.
- Numerical stability is guaranteed.
- It maintains N-space without use of state space equation.
- Eigenpair derivatives are obtained simultaneously.
- It requires only corresponding eigenpair information.
- Numerical stability is guaranteed.
• Combining eq.(13) and eq.(14) into a single equation
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 1616
Second-order eigenpair derivatives of damped systemwith repeated eigenvalues
• Differentiating eq.(13) w.r.t. another design parameter β
(16)
(17)
mmmmmmmmm
mmmmmmmm
mmmm
MX2X)G~
G~
F~~
(
X)GF~
(X)GF~
(
X)CM2()KCM(
,,,,,,,
,,,,,,
2
,Xm ,m
• Differentiating eq.(14) w.r.t. another design parameter β
mmmmm
mmmm
mmmmmmm
mmmm
X)M2M2G~
(X5.0
X)M2G~
(X
X)M2G~
(XXGX
MXX)CM2(X
,,,,,T
,,,T
,,,T
,T
,
TT
,Xm ,m
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 1717
• Combining eq.(16) and eq.(17) into a single equation
mmmmm
mmmmmmmmmmm
mmmmmm,mm,m
mmmmmmmm
m
m
mmmm
mmmm
X)M2M2G~
(X5.0
X)M2G~
(XX)M2G~
(XXGX
MX2X)G~
G~
F~~
(
X)GF~
(X)GF~
(
X
MXXCM2(X
X)CM2(KCM
,,,,,T
,,,T
,,,T
,T
,
,,,,,
,,,,,,
,
,
TT
2
(18)
where
,,,2
,
,,,2
,
2
KCMF~~
KCMF~
KCMF
mmm
mmm
mmm
,,,
,,,
CM2G~~
CM2G~
CM2G
mm
mm
mm
mmm
mmm
m
m
mmmm
mmmm
X)CM2(X5.0
X)KCM(
X
XMX)CM2(X
X)CM2(KCM
,,T
,,,2
,
,
TT
2
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Numerical stability of the proposed method
)det()det()det()det( YAYYAY *T*T
Determinant property
x
]xxx[X]xxx
I0
0Y
A
m21m21mn2
m
r eigenvectoadjacent oft independen
be chosen to t vectorsindependenArbitrary :
when [
singular-non :
eq.(15) ofmatrix t coefficien The : where
i
1
*
(19)
Structural Dynamics & Vibration Control Lab., KAIST, KoreaStructural Dynamics & Vibration Control Lab., KAIST, Korea 1919
00
0A~
)KCM( 2Tmm where
T
T
T
I
B~
)CM2(X
I
B~
X)CM2(
m
mm
m
mm
Then,
(20)
mmmm
mmmm
mmmmm
mmmm
m
XMX)CM2(X
X)CM2()KCM(
I
Ψ
XMX)CM2(X
X)CM2(KCM
IYAY
T
T2T
TT
2*T
T
(21)
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• Arranging eq.(20)
mmm
m
MXXIB~
I00
B~
0A~
YAYTT
*T
0)A
~(det
B~
0A~
B~0
MXXI
I0det)A
~(det
Y)A(Ydet
1
TT
*T
mmm
m
(22)
• Using the determinant property of partitioned matrix
(23)
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0)A(det *
Therefore
Numerical Stability is Guaranteed.Numerical Stability is Guaranteed.
(24)
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80 : DOF ofNumber
20 : elements ofNumber
21 : nodes ofNumber
Data System
0.001 :dampingRayleigh
kg/m 10.887 :density Mass
N/m 102.10E : Modulus sYoung'33
211
Properties Material
)01.0w/ww ( : parameter Design*
z
y
z
mL 10 mw 5.0
mh 05.0x
x
z
y
1
2
3 4
Cantilever beam
NUMERICAL EXAMPLE
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Results of analysis (eigenvalues)
Modenumber
EigenvaluesFirst derivatives
of eigenvaluesSecond derivatives
of eigenvalues
1, 2-1.4279e-03
±j5.2496e+00-2.8057e-10
j3.5347e-104.3916e-09
±j1.0285e-08
3, 4-1.4279e-03
±j5.2496e+00-2.2756e-02
±j5.2494e+01-2.7553e-01
j6.1102e-02
5, 6-5.4154e-02
±j3.2895e+01-6.6265e-10±j2.3445e-10
1.0084e-08 j2.4918e-09
7, 8-5.4154e-02
±j3.2895e+01-1.0818e+00±j3.2886e+02
-1.0391e-08 j2.6913e+00
9, 10-4.2409e-01
±j9.2090e+016.9247e-10
j6.9600e-10-1.0391e-08±j1.1514e-08
11, 12-4.2409e-01
±j9.2090e+01-8.4753e+00±j9.2029e+02
-8.4535e+01 j1.8358e+01
±
±
±
±
±
±
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Results of analysis (first eigenvectors)
DOFnumber
EigenvectorsFirst derivatives of eigenvectors
Second derivatives of eigenvectors
1 0 0 0
2 0 0 0
3-6.6892e+05-j6.6892e+05
3.3446e-04+j3.3446e-04
-5.0169e+03-j5.0169e+03
4-2.6442e+04-j2.6442e+04
1.3221e-03+j1.3221e-03
-1.9596e+02-j1.9596e+02
77 0 0 0
78 0 0 0
79-1.5577e+02-j1.5577e+02
7.7887e-02+j7.7887e-02
-1.1683e+00-j1.1683e+00
80-2.1442e+03-j2.1442e+03
1.0721e-02+j1.0721e-02
-1.6082e+01-j1.6082e+01
… … … …
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Results of analysis (errors of approximations)
Mode number
ActualEigenvalues
Approximated eigenvalues
Variations of eigenpairs Errors of approximations
Eigenvalues Eigenvectors Eigenvalues Eigenvectors
1, 2-1.4279e-03
±j5.2496e+00-1.4279e-03
±j5.2496e+002.2281e-11 4.9628e-03 2.2283e-11 3.7376e-05
3, 4-1.4556e-03
±j5.3021e+00-1.4555e-03
±j5.3021e+001.0000e-02 9.9010e-03 2.6622e-08 1.0000e-04
5, 6-5.4154e-02
±j3.2895e+01-5.4154e-02
±j3.2895e+013.7084e-12 4.9628e-03 3.6899e-12 3.7376e-05
7, 8-5.5241e-02
±j3.3224e+01-5.5236e-02
±j3.3224e+019.9997e-04 9.9023e-03 1.6763e-07 1.0001e-04
9, 10-4.2409e-01
±j9.2090e+01-4.2409e-01
±j9.2090e+019.1400e-12 4.9628e-03 9.1432e-12 3.7376e-05
11, 12-4.3261e-01
±j9.3010e+01-4.3256e-01
±j9.3010e+019.9936e-03 9.9041e-03 4.6508e-07 1.0002e-04
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CONCLUSIONS
Proposed Method Proposed Method
is an efficient eigensensitivity method for the damped system with repeated eigenvalues
guarantees numerical stability
gives exact solutions of eigenpair derivatives
can be extended to obtain second- and higher order derivatives of eigenpairs
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An efficient eigensensitivity method for the An efficient eigensensitivity method for the
damped system with repeated eigenvaluesdamped system with repeated eigenvalues
Thank you for your attention!Thank you for your attention!