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    Feedback-Linearization-Based Nonlinear Controlfor PEM Fuel Cells

    Woon Ki Na, Student Member, IEEE, and Bei Gou, Member, IEEE

    AbstractThis paper presents a dynamic nonlinear model forpolymer electrolyte membrane fuel cells (PEMFCs). A nonlinearcontroller is designed based on the proposed model to prolong thestack life of the PEM fuel cells. Since it is known that large devi-ations between hydrogen and oxygen partial pressures can causesevere membrane damage in the fuel cell, feedback linearizationis applied to the PEM fuel cell system so that the deviation can bekept as small as possible during disturbances or load variations. Adynamic PEM fuel cell model is proposed as a nonlinear, multiple-input multiple-output system so that feedback linearization canbe directly utilized. During the control design, hydrogen and oxy-gen inlet flow rates are defined as the control variables, and thepressures of hydrogen and oxygen are appropriately defined as the

    control objectives. The details of the design of the control schemeare provided in the paper. The proposed dynamic model was testedby comparing the simulation results with the experimental datapreviously published. The simulation results show that PEMFCsequipped with the proposed nonlinear controls have better tran-sient performances than those with linear controls.

    Index TermsExact linearization, nonlinear dynamic model,polymer electrolyte membrane fuel cells.

    I. INTRODUCTION

    A

    FUEL cell is an electrochemical energy device that con-

    verts the chemical energy of fuel directly into electricity

    and heat with water as a by product of the reaction. As a renew-able energy source, the fuel cell is widely regarded as one of the

    most promising energy sources because of its high energy effi-

    ciency, extremely low emission of oxides of nitrogen and sulfur,

    and very low noise, as well as the cleanness of its energy pro-

    duction. Based on the currently used types of electrolytes, fuel

    cells are divided into polymer electrolyte membrane fuel cells

    (PEMFCs), solid oxide fuel cells (SOFCs), phosphoric acid fuel

    cells (PAFCs), molten carbonate fuel cells (MCFCs), alkaline

    fuel cells (AFCs), direct methanol fuel cells (DMFCs), zinc air

    fuel cells (ZAFCs), and photonic ceramic fuel cells (PCFCs) [1].

    In order to generate a reliable andefficient powerresponseand

    to prevent membrane damage as well as detrimental degradationof the stack voltage and oxygen depletion, it is necessary to de-

    sign a better control scheme to achieve optimal air and hydrogen

    inlet flow ratesi.e., controls that can perform air and hydrogen

    pressure regulation and heat/water management precisely based

    on the current drawn from the fuel cell system [3], [4].

    Manuscript received March 24, 2007; revised June 4, 2007. Paper no.TEC-00091-2006.

    The authors are withthe Energy System Research Center,University of Texas,Arlington, TX 76019 USA (e-mail: [email protected]).

    Color versions of one or more of the figures in this paper are available onlineat http://ieeexplore.ieee.org.

    Digital Object Identifier 10.1109/TEC.2007.914160

    Fig. 1. Polarization curve (Ballard Mark V PEMFC at 70

    C) [1].

    First of all, an PEMFC system must be accurately modeled in

    order to apply a suitable nonlinear control scheme. Models have

    been reported so far in the literature for the PEMFC, ranging

    from stationary and dynamic models [3][9], [13][17], [20],

    [24] for the control design applied to a fuel cell vehicle and a

    distributed generation system [11], [12].

    Unfortunately, those models are mainly for experimental ver-

    ifications other than control design [1][3] or for prediction of

    the fuel cell phenomenon by analyzing an electrochemical re-

    action, the thermodynamics, and the fluid mechanics. Recently,Purkrushpan et al. [3] developed a control-oriented PEMFC

    model that includes flow characteristics and dynamics of the

    compressor and the manifold (anode and cathode), reactant par-

    tial pressures, and membrane humidity. However, because of

    the nonlinear relationship between stack voltage and load cur-

    rent shown in Fig. 1 [1] and the state equations [3], [20], it is

    a challenge to develop a nonlinear controller for the PEMFC.

    Because of the operational parametric uncertainties such as the

    parametric coefficients for each cell on kinetic, thermodynamic,

    and electrochemical foundations, and the resistivity of the mem-

    brane for the electron flow, the linear PEMFC models proposed

    by Purkrushpan and coworkers [3][5] and Chiu et al. [20]

    using Jacobian linearization via a Taylor series expansion at

    the nominal operating point cannot easily achieve satisfactory

    dynamic performance under large disturbances. An accurate

    nonlinear dynamic model needs to be developed for the fuel

    cell system as well as an advanced controller design technique,

    considering the nonlinearity and uncertainty that need to be

    proposed.

    A fuzzy control system for a boost dc/dc converter of a fuel

    cell system was developed in [18]. Neural optimal control was

    presented for the PEMFC by using an artificial neural network

    (ANN) in [19]. However, instead of controlling the PEM fuel

    cell system, the neural optimal control is mainly used to derive a

    new architecture to synthesize an approximated optimal control

    0885-8969/$25.00 2008 IEEE

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    by means of the ANN, where the PEM fuel cell was chosen as

    a test bed.

    In this paper, feedback linearization, a well-known nonlinear

    approach, is applied to design a controller, based directly on

    the nonlinear dynamic fuel cell model, to achieve more robust

    transient behavior. Furthermore, the fuel cell stack life can be

    prolonged and stack systems can be protected by minimizing thedeviations between the hydrogen and oxygen partial pressures

    [2], [4].

    In the last few years, feedback linearization for nonlinear dy-

    namic models has been widely used [26][29], [31]. Feedback

    linearization uses a nonlinear transformation to transform an

    original nonlinear dynamic model into a linear model by diffeo-

    morphism mapping [26][29], [31]. An optimal control theory

    is also applied to obtain a linear control that is transformed back

    to the original space by using the nonlinear mapping.

    In this paper, the nonlinear dynamic model developed in

    [3][5] and the small signal model of an PEMFC in [20] are

    considered together to obtain a new dynamic nonlinear model

    that is appropriate for developing a nonlinear controller. Theproposed controller, which is expected to perform rapid tran-

    sient responses under load variations, is tested in MATLAB

    simulink environment.

    The paper is organized as follows. Section II gives a brief

    introduction to feedback linearization. The PEMFC dynamic

    model based on [3][5] and [20] is proposed in Section III, and

    Section IV addresses the design of a nonlinear controller for

    an PEMFC. Section V provides the simulation results for the

    proposed controller, and Section VI concludes the paper.

    II. NONLINEAR CONTROL BY FEEDBACK LINEARIZATION

    For decades, significant progress has been made in control

    designs based on nonlinear concepts. In particular, nonlinear

    control theory developed from differential geometry, known as

    exact linearization or feedback linearization, has become more

    and more attractive for chemical process control because many

    chemical processes are basically of high nonlinearity [29], [34].

    Hence, one of the main motivations of utilizing feedback lin-

    earization for a fuel cell system is that the operation of PEMFC

    is inherently a nonlinear chemical process. In this section, feed-

    back linearization of nonlinear systems is briefly introduced.

    More details of nonlinear control based on differential geome-

    try are available in [26][28], [34].

    A. Feedback or Exact Linearization

    Consider a single-input single-output (SISO) nonlinear sys-

    tem described by the state equation

    x = f(x) + g(x)u

    y = h(x) (1)

    where x is an n-dimensional state vector that is assumed to be

    measurable, u is a scalar input, and y is a scalar output.

    The objective of feedback linearization is to create a linear

    differential relation between the output y and a newly defined

    input v. The notation and concepts of differential geometry are

    essential to understand this approach.

    The Lie derivative of a scalar function h(x) with respect to a

    vector function f(x) is defined as

    Lfh(x) = hf =h(x)

    xf(x). (2)

    Repeated Lie derivatives can be defined recursively as

    Lkfh(x) = Lf

    Lk1f h

    =

    Lk1f h

    f

    L0fh(x) = h(x) (3)

    fork = 1, 2, . . .Similarly, in case of another vector field g

    Lg Lfh = (Lfh)g. (4)

    The output needs to be differentiated for r times until it is

    directly related to the input u. The numberris called the relative

    degree of the system.The system is said to have a relative rat a point x0 if1) Lg L

    kfh(x) = 0 for all xin the neighborhood ofx0 and for

    k < r 1;2) Lg L

    r1f h(x0 ) = 0.

    Thus, according to the aforementioned condition, with a de-

    fined relative degree, the r time derivatives of y are described

    as

    y(k ) = Lkf(x)h(x), fork = 0, 1, . . . , r 1,

    y(r ) = Lrf(x)h(x) + Lg Lr1f h(x)u. (5)

    The control law is

    u =1

    Lg Lr1f h(x)

    Lrfh(x) + v

    (6)

    where y(r ) = v. This control law can transform the nonlinearsystem into a linear one. In addition, a nonlinear transformation

    of a coordinate in the state space

    z = (x) (7)

    is called a local diffeomorphism, in which the map between

    the new input v and the output is exactly linear for all x in the

    neighborhood ofx0 .This feedback linearization theory can be used to design

    multiple-input multiple-output (MIMO) nonlinear system:

    x = f(x) +m

    i=1

    gi (x)ui

    yi = h(x), i = 1, 2, . . . , m (8)

    where x is an n-dimensional state vector and u and y are m-

    dimensional input and output vectors. The system is said to

    have a vector relative degree {r1 , r2 , . . . , rm } at a point x0 if1) Lgj L

    kfhi (x) = 0 for all 1 j m, all 1 i m, k