Authors:
Kartik B. Ariyur,
Andrzej Banaszuk,
Miroslav Krstić,
Volume: 1, Page 2017 Paper number 1667
Abstract:
Attenuation of thermoacoustic oscillations by active control has lately
received considerable attention. In the present work, we identify
the averaged dynamics or the dynamics of the amplitude of a controlled
thermoacoustic instability. The identification is performed on a lean
premixed combustor which has feedback control incorporated to attenuate
the amplitude of the thermoacoustic oscillation. For the purpose of
control, acoustic pressure in the combustor is sensed and fuel flow
actuated by a phase-shifted version of the measured pressure signal.
This control strategy, used by several authors in the literature,
is motivated by the famous Rayleigh criterion for growth/attenuation
of thermoacoustic oscillations. The averaged model we identify consists
of a map of equilibrium amplitudes parametrized by the control phase
shift, to which all the amplitudes settle exponentially fast from all
initial conditions. An equilibrium map is obtained by fitting a curve
through the equilibria equilibria found from steady state experiments,
and decay rates at these equilibria are estimated from cumulative averaging
of several step responses (the steps are in the controller parameter)
to eliminate noise. The identified closed-loop model can be used to
optimize feedback and for simulation studies.
Authors:
Jordan M. Berg,
Nan Zhou,
Volume: 1, Page 2023 Paper number 2157
Abstract:
This paper considers the problem of determining a finite number of
discrete parameters appearing in a nonlinear partial differential equation
describing a curve evolution process. The method is applied to the
plasma etching of thin films for semiconductor manufacturing. Results
are obtained within the mathematical framework of level set methods.
Here, the evolution of the curve under study is captured through the
evolution of a level set function. The underlying physics of the process
are completely contained in a scalar function called the speed function.
The degree of difficulty of treating the evolution equation depends
on the functional dependencies of the speed function. This paper presents
optimal estimation and design techniques based on analytical gradient
computations for a class of position and orientation dependent speed
functions. The technique is demonstrated on a plasma etching model
taken from the literature. Only simulation results are presented here,
but the model under study has been shown to reproduce experimental
data with reasonable accuracy. In the estimation problem, parameters
in the model are fit to best match the feature shape measured in experiments.
In the optimal design problem, parameter values are selected to most
closely attain a desired feature shape.
Authors:
Andreas Johansson,
Alexander Medvedev,
Daniel Widlund,
Volume: 1, Page 2029 Paper number 1867
Abstract:
A nonlinear observer is developed for metal analysis in the top blown
converter process. It is shown that the observer is asymptotically
stable and a region of attraction, where the estimation error converges,
is derived. Using real plant data from the converter at SSAB Oxelösund
AB, the observer is shown to provide accurate estimates of the carbon
content.
Authors:
V. Venkatasubramanian,
Meng Shen,
Volume: 1, Page 2035 Paper number 1975
Abstract:
The paper proposes a new framework for decoupled on-line estimation
of power system dynamic components in the form of input-output models.
Feasibility of the framework is illustrated in the paper by successful
parameter estimation of traditional generator dynamic models in a 39
bus power system.
Authors:
Mats Lundberg,
Per-Johan Nordlund,
Karin Staahl-Gunnarsson,
Volume: 1, Page 2040 Paper number 1063
Abstract:
In future versions of Saab Gripen, the mechanical artificial horizon
will be replaced by a computer calculated attitude and heading, independent
of the inertial navigation system (INS). The system uses data from
sensors already existing in the aircraft, which are easily available
in a highly integrated, 4th generation combat aircraft such as the
Gripen. The sensor information used is a three-axis magnetic detector,
true airspeed, angle of attack, barometric altitude, flight control
rate gyros and load factor. The sensor data is fused together in an
Extended Kalman filter (EKF). Each sensor by itself is of relatively
poor quality. For instance, the accuracy of the rate gyros is in the
order of degrees per second, rather than degrees per hour as is the
case in gyros dedicated for navigational use. However, when all data
are combined, they provide an attitude and heading estimate with sufficient
quality for its purpose; to cross-monitor the INS, and to serve as
a backup in case the INS fails or data can not be displayed. The system
is called Synthetic Attitude and Heading Reference System (SAHRS),
and is a Saab patent. A similar system is developed and operational
in the Saab Viggen.
Authors:
Carlos Canudas de Wit,
Ayman Youssef,
Jean-Pierre Barbot,
Philippe Martin,
Francois Malrait,
Volume: 1, Page 2044 Paper number 1293
Abstract:
The paper studies the observability conditions for the induction motor.
We first review the sufficient condition derived by from the classical
geometrical analysis, then we present some particular case where these
conditions turn out to be also necessary. The purpose of the paper
is to clarify observability problems found in particular when the machine
is operating at low frequencies. The observability analysis also clarifies
the fact that the observability problems are physically due to low
frequency operation conditions, rather than to low rotational speed
operation (even if these two cases coincides in absence of torque load).
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