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Experimental identification of transfer functions for diffusive - - PowerPoint PPT Presentation

Experimental identification of transfer functions for diffusive and/or advective heat transfer for linear time invariant dynamical systems Denis Maillet U niversity of L orraine & CNRS, Nancy, France U niversity of L orraine & CNRS,


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SLIDE 1

Denis Maillet University of Lorraine & CNRS, Nancy, France

Experimental identification of transfer functions for diffusive and/or advective heat transfer for linear time invariant dynamical systems

University of Lorraine & CNRS, Nancy, France Laboratoire d'Energétique et de Mécanique Théorique et Appliquée (LEMTA)

New Trends in Parameter Identification for Mathematical Models IMPA, Rio de Janeiro, Brazil, October 30 – November 3, 2017 Contribution: Waseem Al Hadad

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SLIDE 2

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

2

Experimental inverse problems in heat transfer and engineering METTI Group, SFT (French Heat Transfer Society) Recently: interest in convolutive models and associated inverse problems

* Pollutant source identification in a ventilated domain (turbulence, transient concentration measurements) * Transient thermal behaviour of heat exchanger (PhD W. Hadad, Fives Cryo postDoc) * Virtual sensor construction in a furnace under vacuum conditions (PhD T. Loussouar, Safran Group)

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SLIDE 3

Scope

  • 1. Forced thermal response of Linear advective/diffusive systems with Time Independent

(LTI) coefficients

  • 2. The calibration problem

2.1 Case of a heat exchanger 2.2 Experimental Impedance/transmittance estimation for a half heat exchanger

  • 3. Analysis of deconvolution deadlocks

3.1 Reference case: 1D transient conduction

3

3.1 Reference case: 1D transient conduction 3.2 Noisy matrix and Total Least Squares 3.3 Comparison of calibration methods

  • 4. Rectangular deconvolution

4.1. Point versus averaged values for input and unknown 4.2 Rectangular deconvolution (using « stairs » parameterizing) 4.3 Rectangular estimation with n < m non uniform (NU) time steps

  • 5. Conclusions/perspectives

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 4
  • 1. Forced thermal response of an advective/diffusive system with time constant coefficients

solid - Ω3

Flowing fluid

Material multicomponent system = K solid or fluid domains solid fluid

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

4

Assumptions: time constant thermophysical properties and velocity field

solid - Ω1 solid - Ω4 solid - ΩK

fluid ΩK -1

solid - ΩK-2

Flowing fluid Ω2

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SLIDE 5

Initial uniform state or steady state temperature field + one single separable thermal excitation

solid - Ω1 solid - Ω3 solid - Ω4

Flowing fluid ΩK -1 Flowing

) (t Qv

s

P

init s s

T t T t Q ≠ ) (

  • r

) (

init

T t T ≠

∞ )

(

s

P

(P) h

s

P

) ( ) ( t T c m t Q

in b in in in

& =

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

5

Fixed geometrical support:

  • point
  • line
  • surface
  • volume

solid - ΩK solid - ΩK-2

Flowing fluid Ω2

Time part of thermal excitation u (t) (starts at time t = 0) :

  • volumetretric heat source
  • surface heat or temperature source
  • change of external fluid temperature
  • change of temperature at one fluid inlet

) (t T in

b

init

T t T ≠

∞ )

(

) (

  • r

) ( t T t Q

s s

) (t Qv

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SLIDE 6

P

t coefficien transfer heat (P) v : field velocity (P) : heat volumetric (P) : ty conductivi thermal c r ρ λ

Change of perspective: one single heterogeneous fluid in one single domain (if solid part : zero velocity)

) (t Qv

s

P

init s s

T t T t Q ≠ ) (

  • r

) (

init

T t T ≠

∞ )

(

s

P

(P) h

) ( ) ( t T c m t Q

in b in in in

& & =

6 6

) (P, ) ( t T t y ≡

P

(P) : ) boundaries (external t coefficien transfer heat h

Transient separable thermal excitation :

u (t)

) (P, ) ( t T t y ≡

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

Point response at any point P :

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SLIDE 7

Physical system: Set of solids AND fluid(s): 3D forced convection with constant velocities (in time but not in space) P = ANY point in the system

Recap:

One single thermal excitation defined by its support

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

( ) ( )

( )

(P) ) ( ) (P (P) ) (P (P) P ) (P P

source

f V t Q t , T t , T u c t , t T c

v

+ ∇ ∇ = ∇ + ∂ ∂ r r r r λ ρ ρ . .

Transient Advection Conduction Internal source

Assumptions : Transient heat equation + boundary conditions with time-invariant coefficients + uniform initial temperature or steady state (the system is Linear and also Time-Invariant LITI)

One single thermal excitation defined by its support

7

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SLIDE 8

Assumptions : Transient heat equation + boundary conditions with time-invariant coefficient + uniform initial temperature (the system is Linear and also Time-Invariant LITI)

(P)

  • )

(P ) (P

init

T t , T t , = θ

Temperature rise at any point P:

t t , t p p , d ) (P ) (- exp ) (P θ θ

=

Its Laplace transform :

Laplace parameter

( ) ( )

( )

(P) ) ( ) (P (P) ) (P (P) P ) (P P

source

f V p Q p , p , u c p , p c

v

+ ∇ ∇ = ∇ + θ λ θ ρ θ ρ r r r r . .

Transient Advection Conduction Internal source

( ) ( )

( )

(P) ) ( ) (P (P) ) (P (P) P ) (P P

source

f V t Q t , T t , T u c t , t T c

v

+ ∇ ∇ = ∇ + ∂ ∂ r r r r λ ρ ρ . .

Transient Advection Conduction Internal source

Consequences :Laplace transformed heat equation (no time derivative)

8

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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Linear system with a single excitation Temperature or flux response at any point P in the system ⇒

) ( ) , (P ) (P, p u p H p y = t' ' t u ' t t H t u * t , H t , y

t

d ) ( ) (P, ) ( ) (P ) (P

− = =

  • r convolution product (time domain)

response excitation

= simple product (Laplace domain)

H (P , t)

init , in b in b init s init s init s s init v v

T t T T t T T t T Q t Q Q t Q t u t u

  • )

(

  • r
  • )

(

  • r

) (P

  • )

(

  • r

) (

  • r

) ( ) ( ) (

∞ ∞

− − = : Excitation

) (P, direction any in flux heat local

  • r

(P)

  • )

(P, ) (P, ) ( ) ( t T t T t t y t y

x init

ϕ θ = = : P point specific any in Response

Transfer function

response

9

« init »= initial steady state

  • r uniform temperature field
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SLIDE 10

t

H

t' ' t u ' t t H t u * t , H t , y

t

d ) ( ) (P, ) ( ) (P ) (P

− = =

response excitation

t

) (t u

t

) (t y

) (t H

ss

y

ss

u

Steady state (ss) version

  • f a transfer function

( ) dt

t H u y H

ss ss ss

= =

Time distribution asymptotic values

impedance) (thermal variation) re (temperatu (P) power) (thermal : case Z H T T y Q Q

  • r

Q u

init SS

≡ ⇒ − = ≡ − ≡ θ

Q Z T T

ss ss

= −

Φ R T T

  • ut

in

= −

10

Thermal resistance, flux pipe between 2 isothermal surfaces Generalized resistance, no flux pipe

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 11

T t , T = = ) (P

Constant thermo-physical properties (fluid and walls) and velocities (LTI heat equation) : Assumptions :

= ∂ ∂ t / β

.... , , , u , u

cold hot

ρ λ β ≡ Uniform initial conditions/initial steady state)

  • 2. The calibration problem

2.1 Case of a heat exchanger

(P) ) (P

ss

T t , T = =

init

T t , T = = ) (P

( ) ( )

init q q

T t T t − = θ

Transient/unsteady thermal regime with observed responses at any point q :

( ) ( )

and ≠ > = ≤ t t

q q

θ θ

One single heat source (inlet temperature increase) that starts at t = 0+ :

  • )

( ) (

1 1

≠ =

init

T t T t θ

Heat losses through convection/(linearized) radiation with environment through a uniform heat transfer coefficient h at temperature

init

T T =

{

Cause Consequences

  • )

( ) (

4 4

= =

init

T t T t θ

11

(P) ) (P

ss init

T t , T = =

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SLIDE 12

Calculation of convolution products (transmittance case) Parameterizing with piecewise constant functions, square case m / t t m i t i t t

final i

= = = = ∆ ; to 1 for ∆ ;

response unique pseudo source transmittance

(P) ∆ ) (P d ) (P, ) (P, d ) ( ) (P, ) ( ) (P ) (P

1

1 1 1 1 1 j , m j i t t

W t t , ' t ' t W ' t t t' ' t ' t t W t * t , W t ,

j i + −

∑ ∫ ∫

=

≈ − = − = = θ θ θ θ θ θ

) (

1 t

θ

) (

P1 t

θ

t

1

θ

1

t

2

t

m

t

K t

q

θ

1

t

2

t

m

t

K

Heat exchanger

) ( ) (

3 2

t , t θ θ

1

P

  • r

3 2, q =

q

W1

12

( )

(P)

  • r

) ( for ) ( ) ( 2 1 d ) ( ∆ 1

1 1

1

W t z t z t z t t z t z

i i t t i

i i

θ = + ≈ =

1 j =

sampled averaged over 1 time interval

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 13

( ) ( )

1 2 1

P

  • r

4 3 2 , , q , t t

q q q

=           = θ θ M θ 1 1 1 1

) ( ) ( θ W W θ θ

q q q

M M = =

                ≡

− − 1 2 1 1 2 3 1 2 1

∆ ) ( z z z z z z z z z z t

m m m

L O M M M z M

M (z) Lower triangular Toeplitz matrix function

  • f a vector z

( )

(P)

  • r

) ( for ) ( ) ( 2 1 d ) ( ∆ 1

1 1

1

W t z t z t z t t z t z

i i t t i

i i

θ = + ≈ =

        = w w

2 1

M w

          =

, , 2 1 1 1 1

θ θ M θ

13

( )

tm

q

     θ M

First experiment:

  • Calibration (inverse) problem

instantaneous (sampled) values

       

m

w1 M

       

m , 1

θ M

time averaged values

Next experiments:

  • virtual sensor inverse problem

(same as source estimation problem) q

θ ( )

1 1)

(

θ M

q

ˆ

1

W

measured measured estimated

q

θ

( )

1 1 )

(

− q

W M

1

θ ˆ

measured previously estimated estimated

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SLIDE 14

2 i.i.d. and independent noises 1 1 1

and ε θ θ ε θ θ + = + =

exp q q exp q measured

Model for W identification calibration problem:

q q

W θ θ ) ( 1 M =

exact unknown

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

14

  • with discrepancy principle (Morozov)

( )

exp q exp q

ˆ θ θ W

1 1 )

(

= M

  • Ordinary (linear) least squares:

Ill-posed problem: Inversion needs regularization Here: Truncated SVD or 0 order Tikhonov

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SLIDE 15

Practical way of making the inlet temperature vary

3

T

Cold fuid Hot fluid

3

S

h h

1

T

2

T

4

T

x

2

S

1

S ∞

T

P W Z Q

transmittance impedance

1 1

) ( Z Q θ M =

q q

W θ θ

1 1)

( M =

h

T ) (

1 t

θ

) ( to ) (

3 2

t t θ θ

) (

P t

θ

q

W

1

1

Z

) (t Q

Pseudo Source transmittance impedance

15

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 16

2.2 – Experimental Impedance/transmittance estimation for a half heat exchanger

Response : thermocouples d = 50.8 µm

Identification of transmitance using experimental transient measurements (calibration)

16

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SLIDE 17

) (t Tin ) (t Tout

Upper and lower tranquilization chambers

Comparison of identified Z : step or periodical heating

Identification of transfer function using experimental temperature recording:

step heating identified impedances

− Zin Step - Tikhonov − Zout Step - Tikhonov + Zin Periodical – Tikhonov + Zout Periodical – Tikhonov 1)

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

Square periodical heating

( )

  • ut

in

  • ut

in

θ Q Z

  • r

1

  • r

) (

= M 17 + Zout Periodical – Tikhonov

Z (K . J-1 time (s)

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SLIDE 18

heating step

C T

  • 3

20. =

Comparison of identified transmittance W (outlet/inlet): step or periodical heating

  • ut

b in b

θ θ W ) (

1 −

= M

Pseudo-source Response Transmittance

W (s-1)

− Step - TSVD − Step - Tikhonov − Periodical – TSVD − Periodical – Tikhonov

heating periodical square

s period C T

  • 129

5 21 = =

, .

18

time (s)

Oscillations past first peak and for long times, zero initial level hard to recover : Estimation of transmittance W (noisy output and input) more difficult than Z (noisy output only)

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 19

boundary Heat eq. {

t a x ∂ ∂ = ∂ ∂ θ θ 1

2 2

       > = = ∂ ∂ − = > = = ∂ ∂ − = for at ; for at ) ( t x h t t x t q t l θ θ λ ϕ θ λ ϕ

= T t T t

  • )

( ) ( θ

change of variables ) (t W

) (t q ) (

1 t

T

) (

2 t

T

a c and , ρ λ

  • 3. Analysis of deconvolution deadlocks

3.1 Reference case: 1D transient conduction θ θ ≡ ≡ ≡ y , u , W H

19

) ( ) ( ) ( ) ( ) ( ) (

1 2 1 2

t t W t p p W p θ θ θ θ ∗ = ⇔ =       + =

) ( / ) ( sinh ) ( cosh 1 ) (

1

β λ β β l l h L t W a p =

2

β with

Transmittance

ϕ θ ψ ψ ψ

  • r

for d ) (- exp ) ( ) ( = ≡ ∫ t t p t , x p , x

t

Laplace transform initial

{

l ≤ ≤ = = x t for at θ

2 1

θ θ ≡ ≡ ≡ y , u , W H

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 20

Comparison: analytical W and identified W from synthetic profiles (COMSOL)

Identified W by OLS and TLS Analytical Laplace W + numerical inversion of Laplace

) (t W

) (t q ) (

1 t

θ

) (

2 t

θ

a c and , ρ λ

=

θ

.

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

20

( )

s . t C ; s e t

ss ss

t

5 ∆ and 30 30 with 1

1 1

1

= ° = =         − =

θ τ θ θ

τ

2 1 and

from θ θ W

Identified W by OLS and TLS

versus

      + =

) ( / ) ( sinh ) ( cosh 1 ) (

1

β λ β β l l h L t W

Analytical Laplace W + numerical inversion of Laplace

Numerical Inversion of Laplace Transforms by Hoog’s algorithm Input :

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SLIDE 21

Comparison: analytical W and identified W from synthetic profiles (COMSOL) Comparison without noise:

Validation without committing an INVERSE CRIME

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

21

Temperature profiles (COMSOL)

Analytical and identified W (without regularization)

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SLIDE 22

Calibration problem: how to get the best transfer function H (t) at a point P?

t' ' t t H ' t t u t , H * t u t , y

t

d ) ( ) (, ) (P ) ( ) (P − − = =

sampling

) ( with

  • r

) ( u A H A y H u y M M = = =

parameterization

Available information: Model Measurements 3.2 Noisy matrix and Total Least Squares

u

p

u ex

u

r

22

Available information: discrete noisy values

  • f y (P, t) and u (t)

i i i exp

t y t y ε + = ) ( ) (

i i i exp

t u t u τ + = ) ( ) (

noise

Measurements

t

y

exp

y

y

r

noisy matrix

) ( with τ M = + = ⇒

u u exp

ε ε A A

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

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SLIDE 23

H Identification from u and y measurements :

H u y ) ( M =

ˆ r r H and residuals minimum as such

t

u

y

exp

y

y

r

p

u ex

u

r

Total Least Squares (TLS) solution : augmented matrix

( )

[ ]

y u G M =

concatenation

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

23

u y

ˆ r r H and residuals minimum as such

t

G G H r H r H − = = =

∑ ∑

= + = exp G m i m j j i F G TLS

g J ) ( with ) ( ) (

1 1 1 2 2

Frobenius norm: SVD Form of G Regularized form: Truncated TLS ill-posed

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SLIDE 24

Comparison: analytical W and identified W from synthetic profiles (COMSOL) Comparison with noise:

noised

1

θ

3.3 Comparison of calibration methods

24

Temperature profiles (COMSOL)

Analytical and identified W (with regularization)

K , K 1

2 1

= = σ σ

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

slide-25
SLIDE 25

Comparison: analytical W and identified W from synthetic profiles (COMSOL) Comparison with noise:

noised

2

θ

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

25

Temperature profiles (COMSOL)

Analytical and identified W (with regularization)

K , K 1

2 1

= = σ σ

% . /

noised noised

90 3

2 exact 2 2

= − θ θ θ

Noise over signal ratio:

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SLIDE 26

Comparison: analytical W and identified W from synthetic profiles (COMSOL) Comparison with noise:

noised

2 1

θ θ ,

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

26

Temperature profiles (COMSOL)

Analytical and identified W (with regularization)

K 1

2 1

= = σ σ

slide-27
SLIDE 27

Conclusion of this comparison of deconvolution techniques

noised

1

θ K , K 1

2 1

= = σ σ noised

2

θ

K , K 1

2 1

= = σ σ

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

27

  • Noise on the response θ2 more penalizing than

noise on the source θ1.

noised

2 1

θ θ ,

K 1

2 1

= = σ σ

  • The truncated total least squares do not take

into account the convolutive structure of the matrix M (θ1) no improvement of the estimate

  • Important to improve short times values of the

identified TF in a calibration experiment: largest impact on posterior inverse input estimation experiments.

slide-28
SLIDE 28
  • 4. Rectangular deconvolution

) (t W

) (t q ) (

1 t

θ

) (

2 t

θ

a c and , ρ λ

=

θ

.

Calibration problem : Calibration = model identification for a given structure

) ( with

1 2

θ A W A θ M = =

m output data n =m unknowns m input data

Can the ill-posed problem be more parsimonious ? Less many unknowns n than output data: n << m

Idea: tayloring the definition

  • f the estimate

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

28

2 paths deserve to be investigated BEFORE regularization: Rectangular parametrization using piecewise constant parametrization for W ARX model construction (perspective) Calibration = model identification for a given structure

m input noisy data

exp 2

θ

m output noisy data

exp 1

θ

Parameterization/sampling :

  • W ,θ 1 : piecewise constant functions,

n parameters each

  • θ 2 : m sampled values

Reduced model structure Regularization

reg

W ˆ

Regularized estimate

slide-29
SLIDE 29

noise its

  • n

and

  • f

zation parameteri

  • f

type

  • n

depending ) (

  • f

values Singular

1 1

θ θ M

10

  • 5

10 10

5

lar values (1/s)

(red)

1 sampled

θ (black)

1 stairs

θ

with noise no noise

T

V S U θ = ) ( 1 M

4.1. Point versus averaged values for input and unknown

200 400 600 800 1000 1200 1400 10

  • 20

10

  • 15

10

  • 10

singular value order singular

no noise with noise

( ) ( )

) ( cond ) ( cond

1 1

ampled, 1 , 1 σ α σ α s , stairs ,

θ θ M M ≥

α : truncation order - σ1 = noise level

( ) ( )

) ( ) (

1 1

ampled, 1 1 , 1 1 σ α σ α s , stairs ,

s s θ θ M M ≈

( )

m s / s

,

≤ ≤ = α

α α

1 for ) ( cond

1 1

θ M

slide-30
SLIDE 30

Sampled = parameters = instantaneous value (parameterization over a basis of « hat » functions) : zi = z(ti) Parameterized = averaged value (parameterization over a base of « doors » functions) : zi = 0.5 (z(ti) + z(ti-1))

8 10 x 10

  • 3

(1/s)

ZOOM

Exact W: sampled (continuous) and parameterized (stairs) Estimated W: sampled (continuous) and parameterized

W z

  • r

for

1

θ =

Effect of the type of parameterization: noise on θ 2 only

30

100 200 300 400 500 600 700

  • 2

2 4 6 time t (s) Estimated transmittance W (1

: noise no

2 1

= = ε ε

K 1 :

  • utput

the

  • n

noise i.i.d.

1 2

= = ε ; σ

Truncated SVD: α = 19 for m = 1400 times

parameterized (stairs)

( )

exact

ˆ β β β − = E ) ( bias

( ) ( )

2 2

, ,

bias bias

σ α σ α sampled stairs

  • pt
  • pt

ˆ ˆ W W ≤

slide-31
SLIDE 31

4.2 Rectangular deconvolution (using « stairs » parameterizing)

1

  • r θ

W z =

31

Less many parameters than measurement times: n << m Simplest method = use of a basis of n piecewise constant functions : m/n = c (integer) t0 =0 time

Same time step for measurements and parameterization Parameterization time step larger than measurement one

t’0 =0

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

slide-32
SLIDE 32

Square model :

square square square

W A W θ θ = = ) (

1 2

M

m x m m x 1 m x 1 m x m

[ ]

n

A A A A L

2 1

=

sensitivity matrix sensitivity vectors

Rectangular model :

W X W θ θ = =

square gular tan rec

) ( 1

2

M c = 3

t’j

.

z’j+1 z’j z’j+2 z’j+3 z’j+4z’j+5 z (t) zk zk+1

. . . . . .

t’j-1 t’j+1 t’j+5

t

tk tk +2 tk +1

1

  • r θ

W z =

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

32

sensitivity matrix sensitivity vectors

[ ]

n

X X X X L

2 1

=

m x 1 m x n m x 1 n x 1 m x n

repetition of some lines

                      =

+ − + 1 1 1 1 1

j m , j , j , j

t θ θ θ M M A

+ − =

=

c k c k j j k

c

1 ) 1 (

1 A X

The n rectangular sensitivity vectors are simply the averaged values of the m square sones

local averaging m x 1 n x 1 m x n

W G W =

square

W X W G A θ = =

gular tan rec 2 m x 1 m x n n x 1 m x n

slide-33
SLIDE 33

Effect of rectangular inversion: 1 unknown every c =16 time steps

2 4 6 8 10 x 10

  • 3

: noise no , estimation r rectangula & square

2 1

= = ε ε K 1 :

  • utput

the

  • n

noise i.i.d.

1 2

= = ε ; σ

Square Truncated SVD: α = 19 for n = m = 1400 times

Rectangular TSVD, for n = 87

ated transmittance W (1/s)

33

Rectangular case with n = 87 unknowns

2530 ) ( cond = A

100 200 300 400 500 600 700

  • 2

Estimate time t (1/s) No gain in term of estimation bias % . / ˆ

  • pt

ed recalculat , square

88 3 ) (

1 2

2 2 2

= −

σ α σ

θ W θ θ

% . / ˆ

OLS ed recalculat , gular tan rec

88 3 ) (

1 2

2 2 2

= −

σ σ

θ W θ θ

Same relative RMS residual

slide-34
SLIDE 34

5000 6000 7000 8000 9000

ensitivity vector (1/s)

k

X

(rectangular case, n = 87 sensitivity vectors) low sensitivity

Study of the norm (length) of the sensitivity vectors

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

34 100 200 300 400 500 600 700 1000 2000 3000 4000 5000

time relative to each sensitivity vector (s) Norm of each sen

j

A

(square case, m = 1400 sensitivity vectors) low sensitivity to long times estimates

slide-35
SLIDE 35

4.3 Rectangular estimation with n < m non uniform (NU) time steps

W X θ

NU NU , gular tan rec

=

[ ]

NU

X X X X where ≡

∑ = =

− = +

1 1 1

where 1

1

k ' k k k a a j k NU k

c a c

k k

A X

                      =

+ − + 1 1 1 1 1

j m , j , j , j

t θ θ θ M M A

Each of the n rectangular sensitivity vectors are simply the averaged values of ck square ones

Different number of elementary time steps

35

local averaging lower triangular Toeplitz matrix (square) m x n m x n m x m

) ( with

1 2

θ G A G X W X θ M

NU NU NU NU NU , gular tan rec

= = =

m x n n x 1 m x 1

[ ]

n NU

X X X X L

2 1

where ≡

Question: how to chose the n limits of the n different time steps ?

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

slide-36
SLIDE 36

5000 6000 7000 8000 9000

sensity vectors (1/s)

First try: constant level past time t = 400 s (steady state reached)

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

Study of the norm (length) of the sensitivity vectors

k

X

(rectangular case, n = 87 sensitivity vectors)

NU k

X

36

100 200 300 400 500 600 700 1000 2000 3000 4000

time interval relative to each sensitivity vector (s) Norms of the se

sensitivity vectors) (NU rectangular case, n = 51 sensitivity vectors)

j

A

(square case, m = 1400 sensitivity vectors)

slide-37
SLIDE 37

2 4 6 8 10 x 10

  • 3

mated transmittance W (1/s) Rectangular TSVD, NU case, n = 51, 18 singular values kept Exact W, m = n = 1400

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

37

100 200 300 400 500 600 700

  • 2

time t (1/s) Estimate Rectangular TSVD, for n = 87, 19 singular values kept zoom Improvement of zero level and of the transmittance for short times

slide-38
SLIDE 38
  • 5. Conclusions/perspectives

Importance and applicability of transfer functions (impedances, transmittances, …) in (exact) reduced convolutive model structures for Linear Time Invariant physical systems (detailled model = PDE, integro-differential equations, …) Convolution products can be given a commutative vector/matrix form in discrete time

Denis Maillet, Waseem Al Hadad, New trends in parameter identification, IMPA, Rio de Janeiro, Brasil , oct.-nov.20 17

38

ill-posed inverse problems: identification problem (calibration) first, inverse input problem (source estimation) or inverse (or direct) virtual sensor, or use in a Non Destructive Testing procedure next Path to improve the quality of estimation of transmittance: rectangular deconvolution and pertinent way of tayloring its unknown parameters Perspective: use of ARX structures (AutoRegressive models with eXternal inputs) for better estimation of transfer functions

slide-39
SLIDE 39

Muito obrigado!

39

slide-40
SLIDE 40

2 i.i.d. and independent noises 1 1 1

and ε θ θ ε θ θ + = + =

exp q q exp q measured

Model for W identification calibration problem:

q q

W θ θ ) ( 1 M =

exact unknown

( )

exp q exp q

ˆ θ θ W

1 1 )

(

= M

( )

m T exp

s s s θ L

2 1 1

diag with ) ( = = S V S U M

  • TSVD:

( )

1 1 1 diag with

1 1

L L s / s / s / ˆ

exp T q

= =

− −

S θ U S V W

  • SVD decomposition of square sensitivity matrix:
  • Ordinary least squares:

singular values

Ill-posed problem: Inversion needs regularization Here: Truncated SVD or 0 order Tikhonov

40

  • TSVD:
  • Zero order Tikhonov:
  • r:
  • Choice of the hyperparameters γ = α or µ by discrepancy principle (Morozov) :

( )

1 1 1 diag with

2 1 1 1

L L

α α α α

s / s / s / ˆ

exp q T q

= =

− −

S θ U S V W

( )

W θ θ W r W W r W

W

) ( ) ( where ) ( min Arg

1 2 2 2 2 exp exp q q

ˆ M − ≡       + = µ

µ

        + + + = = =

− − 2 2 2 2 2 2 2 2 2 1 2 2 1 1 1

diag where with

m m exp q T q

s s s s s s ˆ µ µ µ

µ µ µ µ µ

L F S F S θ U S V W

2 2 2

) ( σ

γ

m ˆ ≈ W r

  • rdinary

least squares sum residual vector standard deviation of

q

ε

slide-41
SLIDE 41

Total Least Squares (TLS) solution : augmented matrix

u y

ˆ r r H and residuals minimum as such

G G H r H r H − = = =

∑ ∑

= + = exp G m i m j j i F G TLS

g J ) ( with ) ( ) (

1 1 1 2 2

ˆ

( )

[ ]

y u G M =

concatenation

u

exp

y

p

u ex

u

r

41

( )

      = − =

2 2 2 2 2 2 2

22 21 12 11 2 22 22 12

with

α α α α α α α

V V V V V V V V H

T TLS T

ˆ

SVD form Regularized form: T-TSVD

      = ∑ = − =

− 22 21 12 11 exp 1 12

and with

22

v v ˆ

T TLS

V V V V V U G V H

ill-posed

t

y

y

r

slide-42
SLIDE 42

z (t) = W (t) or θ 1 (t) : defined on a basis of m piecewise constant functions θ 2 : vector of m sampled values

                ≡

− − 1 2 1 1 2 3 1 2 1

∆ ) ( z z z z z z z z z z t

m m m

L O M M M z M

Back to phe parameterization problem

W θ θ ) (

1 2

M =

[ ]

) ( H

  • )

( H ) (

1 1 j j m j j

t t t t z t z − − =

− =

Heaviside function

4.1. Point versus averaged values for input and unknown

42

W z t z z

i i

  • r

for ) (

1

θ = =

Other choice (sampled values)

( )

5 1

10 05 2 ) ( cond .

sampled

= ⇒ θ M

( )

W z t z t z t t z t z

i i t t i

i i

  • r

for ) ( ) ( 2 1 d ) ( ∆ 1

1 1

1

θ = + ≈ =

( )

8 1

10 64 3 ) ( cond .

stairs

= ⇒ θ M