MPC Concepts

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    Lecture 14 - Model Predictive ControlPart 1: The Concept

    History and industrial application resource: Joe Qin, survey of industrial MPC algorithms

    http://www.che.utexas.edu/~qin/cpcv/cpcv14.html

    Emerging applications

    State-based MPC Conceptual idea of MPC

    Optimal control synthesis

    Example Lateral control of a car

    Stability

    Lecture 15: Industrial MPC

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    MPC concept MPC = Model Predictive Control

    Also known as DMC = Dynamical Matrix Control

    GPC = Generalized Predictive Control

    RHC = Receding Horizon Control

    Control algorithms based on

    Numerically solving an optimization problem at each step

    Constrained optimization typically QP or LP

    Receding horizon control

    More details need to be worked out for implementation

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    Receding Horizon Control

    At each time step, compute control by solving an open-loop optimization problem for the prediction horizon

    Apply the first value of the computed control sequence

    At the next time step, get the system state and re-compute

    future input trajectory predicted future output

    Plant

    Model

    prediction horizon

    prediction horizon

    Receding Horizon Control concept

    current dynamic

    system statesPlant

    RHC

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    Current MPC Use Used in a majority of existing multivariable control

    applications Technology of choice for many new advanced multivariable

    control application

    Success rides on the computing power increase

    Has many important practical advantages

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    MPC Advantages Straightforward formulation, based on well understood

    concepts Explicitly handles constraints

    Explicit use of a model

    Well understood tuning parameters

    Prediction horizon

    Optimization problem setup

    Development time much shorter than for competing

    advanced control methods Easier to maintain: changing model or specs does not require

    complete redesign, sometimes can be done on the fly

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    History First practical application:

    DMC Dynamic Matrix Control, early 1970s at Shell Oil Cutler later started Dynamic Matrix Control Corp.

    Many successful industrial applications

    Theory (stability proofs etc) lagging behind 10-20 years.

    See an excellent resource on industrial MPC

    Joe Qin, Survey of industrial MPC algorithms

    history and formulations

    http://www.che.utexas.edu/~qin/cpcv/cpcv14.html

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    Some Major Applications

    From Joe Qin, http://www.che.utexas.edu/~qin/cpcv/cpcv14.html

    1995 data, probably 1-2 order of magnitude growth by now

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    Emerging MPC applications Nonlinear MPC

    just need a computable model (simulation)

    NLP optimization

    Hybrid MPC discrete and parametric variables

    combination of dynamics and discrete mode change

    mixed-integer optimization (MILP, MIQP)

    Engine control

    Large scale operation control problems

    Operations management (control of supply chain) Campaign control

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    Emerging MPC applications Vehicle path planning and control

    nonlinear vehicle models

    world models

    receding horizon preview

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    Emerging MPC applications Spacecraft rendezvous with space station

    visibility cone constraint

    fuel optimality

    Underwater vehicle guidance

    Missile guidance

    From Richards & How, MIT

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    State-based control synthesis

    Infinite horizon optimal control

    ( ) ( )

    0

    1

    22

    )(:subject to

    min)1()()(

    uu

    uuryt

    +

    +=

    )()()1( tButAxtx+=+

    Consider single input system for better clarity

    Solution = Optimal Control Synthesis

    )()( tCxty =

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    State-based MPC concept

    Optimal control trajectories converge to (0,0) IfNis large, the part of the problem for t>Ncan be neglected

    Infinite-horizon optimal control horizon-Noptimal control

    x1

    x2

    t > N

    Optimal

    control

    trajectories

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    State-based MPC Receding horizon control;N-step optimal

    ( ) ( )

    )()(

    )()()1(

    ,)(:subject to

    min)1()()(

    0

    1

    22

    tCxty

    tButAxtx

    uu

    uuryJNt

    t

    =

    +=+

    += +

    +=

    Solution Optimal Control Synthesis

    [ ] )(SolverProblemMPC)( tutx

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    Predictive Model Predictive system model

    +

    +

    =

    )(

    )1(

    Nty

    ty

    YM

    Model matrices

    +

    +

    =

    )(

    )1(

    Ntu

    tu

    U M

    FuHUGxY ++= initial condition response + control response

    )(txx=

    Predicted output Future control input Current state

    (initial condition)

    =

    nCA

    CAG M

    =

    =

    )1()1()(

    0)1()2(

    00)1(

    0

    00

    000

    32 hNhNh

    hh

    h

    BCABCA

    CBH

    NNK

    MOMM

    K

    K

    K

    MOMM

    K

    K

    )(tuu = computed atthe previous step

    +

    =

    )1(

    )3(

    )2(

    Nh

    h

    h

    FM

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    Computations Timeline

    Assume that control u is applied and the state x is

    sampled at the same instant t Entire sampling interval is available for computing u

    x(t)

    t

    x(t+1)

    t+1

    Compute control based

    onx(t). Apply it

    u(t+1)

    time

    u(t)

    Computed at the previous step

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    MPC Optimization Problem Setup MPC optimization problem

    FuHUGxY

    uUDUDrUYYJ

    TTT

    ++=

    +=

    ,:subject tomin

    0

    Solution

    [ ] )1()1(SolverQPProblem,MPC)( UtuUtx =+

    This is a QP problem

    =

    000

    010

    011

    K

    MOMM

    K

    K

    D

    1st difference matrix

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    QP solution QP Problem:

    min2

    1+=

    UfQUUJ

    bAU

    TT

    Standard QP codes can be used

    )(tUU= Predicted

    controlsequence

    HHDrDQ TT +=

    ( )FuGxHf T +=

    =I

    IA0

    1

    1

    ub

    = M

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    Linear MPC Nonlinearity is caused by the constraints

    If constraints are inactive, the QP problem solution isfQU 1

    =

    ( ) ( ))()()1(1

    tFutGxHHHDrDltuTTTT

    ++=+

    =

    0

    0

    1

    Ml

    SuzKxzu 11 +=

    KxSz

    zu

    1

    1

    1

    =

    ( ) GHHHDrDlK TTTT 1+= ( ) FHHHDrDlS TTTT 1+=

    This is linear state feedback

    BuAxzx +=

    Can be analyzed as a linear system, e.g., check eigenvalues

    Ulu T=

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    Nonlinear MPC Stability Theorem - from Bemporad et al (1994)

    Consider a MPC algorithm for a linear plan with constraints. Assume

    that there is a terminal constraint

    x(t+N) = 0 for predicted statex and

    u(t+N) = 0 for computed future control u

    If the optimization problem is feasible at time t,

    then the coordinate origin is stable.

    Proof.

    Use the performance index J as a Lyapunov function. It decreases

    along the finite feasible trajectory computed at time t. Thistrajectory is suboptimal for the MPC algorithm, henceJdecreases

    even faster.

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    MPC Stability The analysis could be useful in practice

    Theory says a terminal constraint is good MPC stability formulations

    (Mayne et al,Automatica, 2000)

    Terminal equality constraint Terminal cost function

    Dual mode control infinite horizon

    Terminal constraint set

    Increase feasibility region

    Terminal cost and constraint set

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    Example: Lateral Control of a Car

    Preview Control MacAdams driver model (1980)

    Consider predictive control design

    Simple kinematical model of a car driving at speed V

    Lane direction

    lateraldisplacement

    y

    x

    V

    u

    Preview horizon

    ua

    aVyaVx

    =

    =

    =

    &

    &&

    sincos

    lateral displacement

    steering

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    Lateral Control of a Car - Model

    Assume a straight lane tracking a straight line

    Linearized system: assume a

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    Lateral Control of a Car - MPC

    Formulate predictive model

    MPC optimization problemFuHUGxY ++=

    = )(

    )()(tytatx

    )()()1( tButAxtx +=+

    =

    = 2

    5.0,

    101

    s

    s

    s VTTB

    VTA

    State-space system:

    Observation: )()( tCxty = [ ]10=C

    ( ) ( )

    ,:subject to

    min

    0uU

    DUDrUFuHUGxFuHUGxJTTT

    +++++=

    [ ] )1()1(QPMPC)( UtuUtx =+ Solution:

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    Impulse Responses

    0 2 4 6 8 10 12 14 16 18 200

    5

    10

    15

    20IMPULSE RESPONSE FOR LATERAL ERROR

    0 2 4 6 8 10 12 14 16 18 200

    1

    2

    3

    4

    5IMPULSE RESPONSE FOR HEADING ANGLE

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    Lateral Control of a Car - SimulationSimulation

    Results:

    V= 50 mph

    Sample time

    of 200ms N= 20

    All variables

    in SI units

    r= 1

    0 1 2 3 4 5 6 7 80

    0.5

    1LATERAL ERROR

    0 1 2 3 4 5 6 7 8-2

    -1.5

    -1

    -0.5

    0HEADING ANGLE (deg)

    0 1 2 3 4 5 6 7 8-1

    -0.5

    0

    0.5

    1STEERING CONTROL (deg/s)

    TIME (sec)

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    Control Design Issues Several important issues remain

    They are not visible in this simulation

    Will be discussed in Lecture 15 (MPC, Part 2)

    All states might not be available

    Steady state error

    Need integrator feedback

    Large angle deviation

    linearized model deficiency

    introduce soft constraint