We present algorithms based on stochastic averaging for estimating nonlinear feedback parameters obtained from time series data with application to noise-driven nonlinear vibration systems, with particular emphasis on limit-cycling thermo-acoustic systems. The harmonic and Gaussian components of relevant signals are estimated from the probability density function (pdf) of an output signal from a single experiment. The respective feedback gains, along with a phase-shifting element are fit to a nominal (given) linear oscillator model from which the parameters of a nonlinearity are fit. When input-output data are available from multiple experiments, the feedback nonlinearity can be estimated point-wise via an iterative algorithm, applicable when the appropriate input signals have a constant (Gaussian) variance. The estimation procedures are demonstrated on a benchmark thermo-acoustic model and applied to time-series data obtained from a limit-cycling combustor rig experiment. In the latter case, relations between the feedback parameters and the fuel to air ratio are briefly discussed.

References

1.
Culick
,
F. E.
, 1976, “
Nonlinear Behavior of Acoustic Waves in Combustion Chambers, Parts I and II
,”
Acta Astronaut.
,
3
, pp.
715
757
.
2.
Banaszuk
,
A.
,
Jacobson
,
C. A.
,
Khibnik
,
A. I.
, and
Mehta
,
P.
, 1999, “
Linear and Nonlinear Analysis of Controlled Combustion Process, Part 2: Nonlinear Analysis
,”
IEEE Conference on Control Applications
,
Kohala Coast, Hawaii
, 22–26 August 1999, Piscataway, NJ, vol.
1
, pp.
206
212
.
3.
Lieuwen
,
T. C.
, 2002, “
Experimental Investigation of Limit-Cycle Oscillations in an Unstable Gas-Turbine Combustor
,”
J. Propul. Power
,
18
, pp.
61
67
.
4.
Lieuwen
,
T. C.
, 2003, “
Statistical Characteristics of Pressure Oscillations in a Premixed Combustor
,”
J. Sound Vib.
,
260
, pp.
3
17
.
5.
Lieuwen
,
T. C.
, and
Banaszuk
,
A.
, 2005, “
Background Noise Effects on Combustor Stability
,”
J. Propul. Power
,
21
(
1
), pp.
25
31
.
6.
Cohen
,
J. M.
, and
Banaszuk
,
A.
, 2003, “
Factors Affecting the Control of Unstable Combustors
,”
J. Propul. Power
,
19
, pp.
811
821
.
7.
Gelb
,
A.
, and Vander
Velde
,
W. E.
, 1968,
Multiple-Input Describing Functions and Nonlinear System Design
,
McGraw-Hill
,
New York
.
8.
Khalil
,
H. K.
, 1996,
Nonlinear Systems
, 2 ed.,
Prentice Hall
,
Englewood Cliffs, NJ
.
9.
Basso
,
M.
,
Genesio
,
R.
, and
Tesi
,
A.
, 1997, “
A Frequency Method for Predicting Limit Cycle Bifurcations
,”
Nonlinear Dyn.
,
13
, pp.
339
360
.
10.
Banaszuk
,
A.
,
Mehta
,
P.
, and
Mezic
,
I.
, 2004, “
Spectral Balance: Frequency Domain Framework for Analysis of Nonlinear Dynamical Systems with Noise
,”
Proceedings of the 43rd IEEE Conference on Decision and Control
, Paradise Island, Bahamas, 14–17 December 2004,
IEEE
,
Piscataway, NJ
, vol.
2
, pp.
2244
2249
.
11.
Roberts
,
J.
, and
Spanos
,
P.
, 2003,
Random Vibration and Statistical Linearization
,
Dover
,
New York
.
12.
Failla
,
G.
,
Spanos
,
P.
, and Di
Paola
,
M.
, 2003, “
Response Power Spectrum of Multi-Degree-of-Freedom Nonlinear Systems by a Galerkin Technique
,”
Trans. ASME, J. Appl. Mech.
,
70
, pp.
708
714
.
13.
Spanos
,
P.
, Di
Paola
,
M.
, and
Failla
,
G.
, 2002, “
A Galerkin Approach for Power Spectrum Determination of Nonlinear Oscillators
,”
Meccanica
,
37
, pp.
51
65
.
14.
Elbeyli
,
O.
, and
Sun
,
J. Q.
, 2002, “
A Stochastic Averaging Approach for Feedback Control Design of Nonlinear Systems Under Random Excitations
,”
Trans. ASME, J. Vib. Acoust.
,
124
, pp.
561
565
.
15.
Balachandran
,
R.
,
Ayoola
,
B.
,
Kaminski
,
C.
,
Dowling
,
A.
, and
Mastorakos
,
E.
, 2005, “
Experimental Investigation of the Nonlinear Response of Turbulent Premixed Flames to Imposed Inlet Velocity Oscillations
,”
Combust. Flame
,
143
, pp.
37
55
.
16.
Cohen
,
J.
,
Hagen
,
G.
,
Banaszuk
,
A.
,
Becz
,
S.
, and
Mehta
,
P.
, 2011, “
Attenuation of Combustor Pressure Oscillations Using Symmetry Breaking
,”
49th AIAA Aerospace Sciences Meeting
,
Orlando, Florida
, 4–7 January 2011.
17.
Teerlinck
,
K. A.
,
Hagen
,
G.
,
Banaszuk
,
A.
,
Lovett
,
J. A.
,
Cohen
,
J. M.
,
Ateshkadi
,
A.
, and
Kiel
,
B. V.
, 2005, “
Demonstration of Thermoacoustic Instability Control in a Three-Flameholder Combustor
,”
53rd JANNAF (Joint Army-Navy-NASA-Air Force) Propulsion Meeting
,
Monterey, CA
, December
5
8
.
18.
Dowling
,
A. P.
, 1997, “
Nonlinear Self-Excited Oscillations of a Ducted Flame
,”
J. Fluid Mech.
,
346
, pp.
271
290
.
19.
Lieuwen
,
T.
, 2005, “
Nonlinear Kinematic Response of Premixed Flames to Harmonic Velocity Disturbances
,”
Proc. Combust. Inst.
,
30
(
2
), pp.
1725
1732
.
20.
Lieuwen
,
T.
, and
Neumeier
,
Y.
, 2002, “
Nonlinear Pressure-Heat Release Transfer Function Measurements in a Premixed Combustor
,”
Proc. Combust. Inst.
,
29
, pp.
99
105
.
21.
Peracchio
,
A.
, and
Proscia
,
W.
, 1998, “
Nonlinear Heat Release/Acoustic Model for Thermo-Acoustic Instability in Lean Premixed Combustors
,”
ASME J. Turbomach.
,
121
, pp.
415
421
, ASME paper 98-GT-269.
22.
Bittanti
,
S.
,
DeMarco
,
A.
,
Poncia
,
G.
, and
Prandoni
,
W.
, 2002, “
Identification of a Model for Thermoacoustic Instabilities in a Rijke Tube
,”
IEEE Trans. Contr. Syst. Technol.
,
10
(
4
), pp.
490
502
.
23.
Mezić
,
I.
, and
Banaszuk
,
A.
, 2004, “
Comparison of Systems with Complex Behavior
,”
Physica D
,
197
, pp.
101
133
.
24.
Murray
,
R.
,
Jacobson
,
C. A.
,
Casas
,
R.
,
Khibnik
,
A. I.
, Johnson Jr., C. R.,
Bitmead
,
R.
,
Peracchio
,
A. A.
, and
Proscia
,
W.
, 1998, “
System Identification of Limit Cycling Systems: A Case Study for Combustion Instabilities
,”
Proceedings of the American Control Conference
, Philadelphia, Pennsylvania, 24–26 June 1998,
IEEE
,
Piscataway, NJ
, pp.
2004
2008
.
25.
Dunstan
,
W.
,
Bitmead
,
R. R.
, and
Savaresi
,
S. M.
, 2001, “
Fitting Nonlinear Low-Order Models for Combustion Instability Control
,”
J. Contr. Eng. Pract.
,
9
, pp.
1301
1317
.
26.
Mehta
,
P.
, and
Banaszuk
,
A.
, 2001, “
On the Identification of a Nonlinear Function in a Feedback Loop
,”
Proc. 40th IEEE Conf. Decis. Contr.
,
5
, pp.
4320
4325
.
27.
Jacobson
,
C. A.
,
Khibnik
,
A. I.
,
Banaszuk
,
A.
,
Cohen
,
J.
, and
Proscia
,
W.
, 2000, “
Active Control of Combustion Instabilities in Gas Turbine Engines for low emissions. Part 1: Physics-Based and Experimentally Identified Models of Combustion Instability
,”
Applied Vehicle Technology Panel Symposium on Active Control Technology
,
Brauschweig, Germany
, 8–11 May 2000,
NATO Research and Technology Organization
, pp.
30
–130–
12
.
28.
Barooah
,
P.
,
Anderson
,
T.
, and
Cohen
,
J.
, 2003, “
Active Combustion Instability Control with Spinning Valve Actuator
,”
Trans. ASME J. Eng.r Gas Turbines Power
,
125
, pp.
925
932
.
29.
Stark
,
H.
, and
Woods
,
J. W.
, 1994,
Probability, Random Processes, and Estimation Theory for Engineers
, 2 ed.
Prentice–Hall
,
Englewood Cliffs, NJ
.
30.
Bendat
,
J. S.
, and
Piersol
,
A. G.
, 2000,
Random Data, and Measurement Procedures
, 3 ed.,
Wiley
,
New York
.
31.
Ljung
,
L.
, 1999,
System Identification Theory for the User
, 2 ed.,
Prentice Hall
,
Englewood Cliffs, NJ
.
32.
Inman
,
D. J.
, 1994,
Engineering Vibration
,
Prentice Hall
,
Englewood Cliffs, NJ
.
33.
Banaszuk
,
A.
,
Mehta
,
P.
,
Jacobson
,
C.
, and
Khibnik
,
A. I.
, 2006, “
Limits of achievable performance of controlled combustion processes
,”
IEEE Trans. Control Syst. Technol.
,
14
(
5
), pp.
881
895
.
34.
Riesz
,
F.
, and
Sz.-Nagy
,
B.
, 1990,
Functional Analysis
,
Dover
,
New York
.
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