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COMPLEX MODES IN LINEAR STOCHASTIC SYSTEMS S. Adhikari Department of Engineering University of Cambridge Trumpington Street Cambridge CB2 1PZ (U.K.) October, 2000 Outline of the Talk Introduction Viscously Damped Systems Complex


  1. COMPLEX MODES IN LINEAR STOCHASTIC SYSTEMS S. Adhikari Department of Engineering University of Cambridge Trumpington Street Cambridge CB2 1PZ (U.K.) October, 2000

  2. Outline of the Talk • Introduction • Viscously Damped Systems • Complex frequencies and modes • System Randomness • Derivatives of Complex Eigensolutions • Statistics of Complex Eigensolutions • Numerical examples • Summary and Conclusions 1

  3. Viscously Damped Systems M ¨ q ( t ) + C ˙ q ( t ) + Kq ( t ) = 0 . (1) where M , C and K are the mass, damping and stiffness matrices respectively. q ( t ) is the vector of generalized coordinates.

  4. Complex Frequencies and Modes The eigenvalue problem associated with equa- tion (1) can be represented by λ 2 k Mu k + λ k Cu k + Ku k = 0 . The eigenvalues, λ k , are the roots of the char- acteristic polynomial s 2 M + s C + K � � det = 0 . The order of the polynomial is 2 N and the roots appear in complex conjugate pairs. The eigenvalues are arranged as s 1 , s 2 , · · · , s N , s ∗ 1 , s ∗ 2 , · · · , s ∗ N . Each complex mode satisfies the normalization relationship u j = 1 � � u T 2 s j M + C ∀ k = 1 , · · · , 2 N , j γ j

  5. System Randomness Randomness of the system matrices has the following form: M = M + δ M , C = C + δ C , and K = K + δ K . Here, ( • ) and δ ( • ) denotes the nominal (deter- ministic) and random parts of ( • ) respectively. It is assumed that δ M , δ C and δ K are zero- mean random matrices. The random parts are small and also they are such that 1. symmetry of the system matrices is pre- served, 2. the mass matrix M is positive definite, and 3. C and K are non-negative definite.

  6. Statistics of the Eigenvalues If the random perturbations of the system ma- trices are small, s j can be approximated by a first-order Taylor expansion as N N N N ∂s j ∂s j � � � � s j = ¯ s j + δK rs + δC rs ∂K rs ∂C rs r =1 s =1 r =1 s =1 N N ∂s j � � + δM rs ∂M rs r =1 s =1 or in a matrix form as   δ K     s − ¯ s = D s δ C  δ M    where ∂s 1 ∂s 2 ∂s N   · · · ∂ K ∂ K ∂ K   ∂s 1 ∂s 2 ∂s N   ∈ R 3 N 2 × N D T   s = · · ·   ∂ C ∂ C ∂ C     ∂s 1 ∂s 2 ∂s N   · · · ∂ M ∂ M ∂ M

  7. Derivatives of Complex Eigensolutions From Adhikari (1999): [ AIAA Journal , 37(11), pp. 1152–1158] Derivative of the j -th complex eigenvalue ∂s j ∂ M ∂ C ∂α + ∂ K � � s 2 ∂α = − γ j u T ∂α + s j u j . j j ∂α Derivative of the j -th complex eigenvector 2 N ∂ u j a ( α ) � ∂α = jk u k k =1 where ∂ M ∂ C ∂α + ∂ K γ j � � a ( α ) u T s 2 = − ∂α + s j u j j k jk s j − s k ∂α ∀ k = 1 , 2 , · · · , 2 N, � = j = − γ j ∂ M ∂α + ∂ C � � a ( α ) 2 u T and 2 s j u j . j jj ∂α

  8. Derivatives w.r.t. the System Matrices For the eigenvalues: ∂s j � � = − γ j U rj U sj ∂K rs ∂s j ∂s j = s j ∂C rs ∂K rs ∂s j ∂s j = s 2 and . j ∂M rs ∂K rs For the eigenvectors: � � 2 N U rk U sj ∂U lj � = − γ j U lk ∂K rs s j − s k k =1 k � = j ∂U lj ∂U lj = − γ j � � U lj + s j U rj U sj 2 ∂C rs ∂K rs ∂U lj ∂U lj � � U lj + s 2 and = − γ j s j U rj U sj . j ∂M rs ∂K rs

  9. Statistics of the Eigenvalues The covariance matrix of the eigenvalues, Σ s is obtained as s ) ∗ T > Σ s = < ( s − ¯ s ) ( s − ¯ T � �    δ K δ K     D ∗ T s = D s Σ kcm D ∗ T     = D s δ C δ C s .  δ M   δ M      Σ kcm ∈ R 3 N 2 × 3 N 2 , the joint covariance matrix of M , C and K is defined as < δ K δ K T > < δ K δ C T > < δ K δ M T >   < δ C δ K T > < δ C δ C T > < δ C δ M T >   Σ kcm =  .    < δ M δ K T > < δ M δ C T > < δ M δ M T >

  10. Statistics of the Eigenvectors For small random perturbations of the system matrices, u j can be approximated by a first- order Taylor expansion   δ K     u j − ¯ u j = D u j δ C  . δ M    D u j , the matrix containing derivatives of u j with respect to elements of the system matri- ces, is given by   ∂U 1 j ∂U 2 j ∂U Nj · · ·  ∂ K ∂ K ∂ K    ∂U 1 j ∂U 2 j ∂U Nj ∈ R 3 N 2 × N   D T u j = · · ·     ∂ C ∂ C ∂ C   ∂U Nj ∂U 1 j ∂U 2 j    · · ·  ∂ M ∂ M ∂ M The covariance matrix of j -th and k -th eigen- vectors u k ) ∗ T > = D u j Σ kcm D ∗ T � � Σ u j u k = < u j − ¯ u j ( u k − ¯ u k .

  11. Numerical example m m k k k m k m k u u u u u u u u u . . . c u c u Linear array of 8 spring-mass oscillators; nominal system: m u = 1 Kg, k u = 10 N/m and c u = 0 . 1 Nm/s

  12. Statistics of the Eigenvalues (a) (b) 7 0.5 0.45 6 0.4 5 0.35 Standard deviation 0.3 4 Mean 0.25 3 0.2 0.15 2 0.1 1 0.05 0 0 2 4 6 8 2 4 6 8 (a) Absolute value of mean of complex natural frequencies (b) Standard deviation of complex natural frequencies; ‘X-axis’ Mode number; ‘—’ Analytical; ‘-.-.-’ MCS

  13. Statistics of the Eigenvectors Mode: 1 Mode: 2 0.5 0.5 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Mode: 3 Mode: 4 0.5 0.5 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Mode: 5 Mode: 6 0.5 0.5 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Mode: 7 Mode: 8 0.5 0.5 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Real part of mean of the complex modes, ‘X-axis’ DOF; ‘—’ Analytical; ‘-.- -’ MCS

  14. Statistics of the Eigenvectors Mode: 1 Mode: 2 0.3 0.3 0.2 0.2 0.1 0.1 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Mode: 3 Mode: 4 0.3 0.3 0.2 0.2 0.1 0.1 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Mode: 5 Mode: 6 0.3 0.3 0.2 0.2 0.1 0.1 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Mode: 7 Mode: 8 0.3 0.3 0.2 0.2 0.1 0.1 0 0 1 2 3 4 5 6 7 8 1 2 3 4 5 6 7 8 Standard deviation of the complex modes, ‘X-axis’ DOF; ‘—’ Analytical; ‘-.-.-’ MCS

  15. Summary and Conclusions • An approach has been proposed to obtain the second-order statistics of complex eigen- values and eigenvectors of non-proportionally damped linear stochastic systems. • It is assumed that the randomness is small so that the first-order perturbation method can be applied. • The covariance matrices of the complex eigensolutions are expressed in terms of the covariance matrices of the system proper- ties and derivatives of the eigensolutions with respect to the system parameters. • The proposed method does not require con- version of the equations of motion into the first-order form.

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