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Robust optimal control of an electro-mechanical system

Citation for published version (APA):

Steinbuch, M., & Bosgra, O. H. (1988). Robust optimal control of an electro-mechanical system. In First Philips conference on applications of systems & control theory (pp. 205-212). Philips Research Laboratories.

Document status and date: Published: 01/01/1988 Document Version:

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Robust Optimal control of an

Electro-Mechanical System

Abstract

M. Steinbuch1 & O.H. Bosgra2

1. Philips Research Laboratories Eindhoven, The Netherlands 2. Delt University of Technology,

Delft, The Netherlands

The control system design for high performance electrcrmechanical systems is investigated. The interaction between the fast dynamics of the electrical part and the slow and structural dynamics of the mechanical part must be accounted for in the control system design. For a wind energy conversion system as an example a multivariable controller is designed. Using the method of optimal output feedback in combination with a multi-model approach, the selection of the controller structure can be used as part of the design process, and robustness is achieved with respect to non- linearities. The results for the wind turbine system are shown, using a non-linear dynamic model, and these are compared to results obtained with a classical PID-controller based design.

Keywords. Electro-mechanical systems. Optimal output feedback. Multi-model robustness.

1

Introduction

A very broad range of products and processes consists of the combination of mechanical and electrical systems. For instance in consumer electronic products, high performance mechanical systems are driven by electrical actuator systems. In the field of energy production, mechanical systems drive electrical generators. Many electro-mechanical systems are interconnected to another process. This process is for instance the optical lightpath in a CD player, or a rotating pair of blades in the case of a wind energy con-version system. The mechanical part is the intermediate between process and actuator or generator part. In the case of precision engineering tools, the process itself is also a mechanical system.

For the control system design for these systems, the classical approach consists of de-signing a controller for the process and the mechanical part first, for instance a turbine speed control in a energy production plant. Separately, the controller for the electrical part is designed. Other systems ( c.f. CD) have multiple loops around the whole sys-tem, designed separately. However, because all the subsystems are interconnected, this

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approach may lead to a low performance. The reason for this is the bilateral coupling (interaction) between the several parts of the controlled system. This means that each subsystem is contained in the cloaed-loop of the other subsystems, and hence can act destabilizing. If the interaction is substantial, a performance increase of the individ-ual controlled loops may result in a decrease of the overall performance, for instance smaller robustness margins.

For this reason an integrated, multivariable approach is needed for the robust control system design, if high performance electro-mechanical systems are required.

2

Problem Formulation

Electro-mechanical systems have several specific properties, such as:

- fast dynamics in the electrical part, which are dominant in the input/output electrical behavior (i.e. both controllable and observable),

- slow mechanical dynamics, in combination with high order structural flexibilities, - high interaction between the subsystems,

- the attached process may be a very nonlinear system with additional dynamics. The control system design on the other hand must realize the performance require-ments, such as:

- stabilization

- high performance, including servo control (tracking) - minimum energy dissipation.

- these requirements must be met under all specified conditions and system param-eter variations (robustness).

The robuatne11 requirement is very important for a high reliability of the process.

Designing for robustness is also very useful for mass-products, such as consumer elec-tronics, to tolerate product variations and thus decrease production costs.

The control problem can now be formulated as designing a robust control system, which

realizes the requirements stated above, and accounts for the system dynamics.

Outline of the paper

In order to be able to solve the control problem a mathematical dynamic model for the system is required. If robustness is to be achieved, it is necessary to have a theoretical model, based on physical laws. In the process of model building the possibility exists to define modelling uncertainties properly, such as high frequency structural modes, which, are to be accounted for in a robust design. Using an experimental modelling setup, only one element of a class of models for the process is obtained, depending on the circumstances under which the measurements have taken place. Nevertheless, system identification can be used to verify the theoretical model or to adjust nominal parameter values. For the design of a multivariable controller several methods exist, such as modal control, optimal control, Invers Nyquist Array. Especially, Linear Quadratic {LQ) optimal control has been shown to be a very powerfull method, with various_ applications in the field of aero-space and power system control. Using LQ control

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with a constrained internal controller structure, in combination with a. multi-model approach, a robust controller can be found which gives a satisfactory performance for a range of operating conditions. For a wind energy conversion system as an example, the design of a robust optimal output feedback will be shown.

3

Wind Turbine Dynamics

The system considered here (Fig. 1) is a three-bladed horizontal axis wind turbine with a rated power of 300 kW. It has a lelatively heavy rotor ( e30m), which is connected with a planetary gear to an electrical conversion system consisting of a synchronous generator, a controllable thyristor bridge rectifier, a DC (ripple) reactor a.nd an inverter.

ROTOR

GEAR GENERATOR RECTIFIER INVERTER GRID

"

s

Fig. 1. Wind energy conversion system

The generator frequency does not depend on the consta.nt grid frequency because of the direct current conversion. Hence, rotor speed w,. is variable which yields a possible increase in energy output and a decrease in meche.nica.l loads. The available inputs are: delay angle a,. of tbe rectifier, field voltage uF of the generator and pitch angle f3

of the blades. The mearured variables are generator speed "' and direct current It1c •

Disturbances acting on the system are wind speed 11, and fluctuations in grid voltage U,. .

Modelling

The wind turbine system can be divided into three main parts: the aerodynamics (forces on the rota.ting blades), the mechanics from rotor to generator-mass and the electrical conversion unit.

The aerodynamic part is modelled using a. non-linear stationary model. It calculates the effective rotor torque as a function of spatial averaged wind speed, rotor speed and pitch angle. The dynamics of the electrical pitch angle excitation 1ystem are decribed using a first order model.

The mechanical part is modelled by a first order lag (rotor and generator inertia) and the second order dynamics of the torsional oscillations resulting from a flexible element in the secondary shaft.

The dynamic1 of the electrical conver1ion 1y1tem, conai1ting of the 1ynchronoU1 gen-erator and tha DC link, a.re very important. The reason is that with the inputs (field

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voltage and delay angle) the mechanical part can be affected very fast. The dynamics of the synchronous generator are described using the Park transformation (Anderson and Fouad, 1982). The model of the DC link consists of the steady-state voltage and phase equations for the converters, as well as a first order model for the intermediate direct current circuit. However, the direct coupling between the generator dynamic equations and the DC load equations results in a set of implicit algebraic and differ-ential equations. A solution is found using an expression for the load angle of the generator, see Steinbuch (1986). This leads to a fifth order dynamic model for the electrical conversion system. Together with the models for the aerodynamic part, for the mechanical part and with additional speed sensor and field excitation actuator dynamics, the complete nonlinear dynamic model is found. It can be written in the

non-linear state-space form dz / dt =

f (

z, u, e ), with z the vector of eleven state

vari-ables (3 mechanical, 5 electrical, 1 pitch servo, 1 field actuator, 1 speed sensor), and

u

=

(/3,uF,a,.) the vector of inputs. The disturbance vector is e

=

(v, Un)· From

this non-linear model, linearized models have been obtained in several operating

con-ditions, written in state-space form: dz/dt

=

Az

+

Bu +Ee, y

=

Oz, with z, u and

y the variations of the original non-linear state, input and output. Matrices A, B, C, and E depend on the operating condition.

Dvnamic Performance

The dynamic performance and characteristics of the wind turbine syste~ is determined

predominantly by the large rotor inertia, the torsional oscillations in the secondary shaft and the fast electrical dynamics (Steinbuch, 1986, 1987). Also, the system is non-linear due to the aerodynamics and the electrical conversion system. Between the

outputs speed and direct current, a large amount of interaction is present, while all the

inputs affect all the outputs. The wind turbine system is therefore a multivariable

sys-tem. The control system should account for these characteristics, in order to meet the

performance requirements. These are for full load conditions ( v ~ 12m/ a): constant

nominal speed and electrical power, low mechanical loads (fatique load: life time), low variations of the inputs. These requirements must be met for a wide range of

operat-ing conditions {12 ~ v ~ 20 m/ a), fast fluctuating wind speed and grid voltage, and

despite a severe restriction on the rate of change of the pitch angle ( d{J / dt ~ 5 o/ s ).

4

Control Methodology

The conflicting requirements make the control problem very suitable for treatment as an optimization problem. A very powerful method, which can handle multivariable systems in a natural way, is the linear quadratic optimal control method (LQ). Appli-cations of this method are widely known in aerospace and power system control. In a previously reported study (Stei:iibuch, 1987) very good results have been obtained with LQ state feedback of the wind turbine. However, in order to design an imple-mentable controller, an output feedback design has to be made. This is possible using observer techniques (c.f. LQG). Nevertheless, due to the high dynamic order of the model and the few number of outputs, this would result in a very complex controller.

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Besides, the non-linearities in the process in combination with strongly fluctuating

wind speeds, would violate the separation principie, possibly resulting in instabilities. Another approach is the use of LQ control with a constrained controller structure.

Parametric optimal control.

Consider the linear model to be controlled:

dz/dt - Az + bu

y - Oz (1)

where z is then-dimensional state vector,~ is them-dimensional input vector, and y is the I-dimensional vector of measured outputs. Suppose system (1) has a nonzero initial condition z(tO) = zO, i.e. we consider the deterministic formulation. The parametric linear quadratic control problem, or optimal output feedback problem, can now be

1tated as finding a controller F such that the quadratic performance index

J =

fo

00

(zTQz

+

uT Ru) dt, is minimized under the constraints

u=Fy,

and the system (1).

Q ~

o,

R

>

0. (2)

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The calculation of the optimal controller Fis possible using equations which are nec-essary conditions for the minimum of (2) to exists, with numerical optimizations pro-grams {Anderson and Moore, 1971; Levine and Athans, 1970; Makila and Toivonen, 1987). The control problem is then reduced to chosing the design parameters Q (control quality), R (control effort) and the initial condition. Using simulations the designer can easily converge to a proper r.hose of these parameters, because they affect the per-formance in a logical way: for instance chosing Q 111 higher will lead to a faster speed control.

The design flexibility offered by the method of optimal output feedback is quite large. Adding integral action to the system {1 ), or general dynamics, a proportional/integral or dynamic feedback can be designed. Putting n additional dynamic orders to (1), the feedback can be split up in an observer and a state feedback controller.

A benefit of the method, in contrast to LQG and Hl techniques, is the possibility of using the internal controller structure as a design tool. Putting some entries of F zero a priori, i.e. deleting some of the feedback paths, and optimizing the other parameters may yield a more simple, robust, decentralized control. In this way, the control system design can be an optimization of the parameters in a classical PID structure, or a full

multivariable feedback, or somewhat in between.

A drawback is that robustness is not obtained a priori. Because the method, as most control design methods, is used for linear aystems, no account is given for non-linearities. In the case of the wind turbine system, especially the aerodynamic part contains non-linear behavior, as well as modelling uncertainties. For this reason a

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Consider the p linear systems:

dz/dt - A(i)z

+

B(i)u,

y - C ( i)z i = 1, ... , p (4)

with the multi-model controller u=Fy, which minimizes the overall performance index:

p

Jeot

=

L

J(i), (5)

i=l

with J(i) calculated using (2) for each system (A(i),B(i),C(i),Q(i),R(i)).

This means that we have one controller F which stabilizes p systems. Therefore, if the non-linear model of the plant is linearized in several operating conditions, it is possible to calculate a robust controller which gives a satisfactory performance in all these conditions.

5

Simulation Results

For the wind turbine system a multi- model robust optimal controller is designed, using proportional an~ integral action, as well as one additional dynamic feedback. The controller uses only 15 out of 24 possible feedback paths. The dynamic behavior of the wind turbine system is simulated using the full non-linear model. The performance is compared to a classical PID design, which is b~ed on a single-input single-output (siso) approach. As a test case, a large wind gust is used (fig. 2a).

In fig. 2c and 2d the responses of the rotor speed and of the electrical power are shown. Both the optimal controller and the siso design control the speed very well (- 13 deviation). However, the power output fluctuations (fig. 2d) differ enormously between both controllers. The siso-design (2) results in 80 kW variation, while the optim&l multivariable controller (1) gives 3 kW (13} fluctuation. Obviously, these variations are also present in the torques, which is undesirable.

The reason for the difference between the controllers is that the multivariable controller compensates for the internal interactions in the wind turbine system, and uses the three inputs in the most efficient way. This can be illustrated with the behavior of the pitch angle (fig. 2b). It is seen from the figure that the optimal controller acts a moment earlier on the pitch angle then the siso controller. This leads to less power variations, despite the restriction in the rate of change of the pitch angle.

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0 Cl

...

...

- -

g..---...---.---...--~-.---~ "'

/

\

..

I

\

y

e.oo 1e.o 24.0 T!HE S

\

'2.0

"°·

0

..

~~+--i+---~----t---+~---+---1 II 8 oo+.---~---+---+---+---1 .... 11... Tl~o 5 z.t.o '2.0 'lll.o

a. wind speed b. pitch angle

2 5'

..

!"' ... _8 o•

...

I

i

2 .:

i

.: O. IXl 11.00 1e.o 2 ... 0 TIHE S

I

i. optimal controller 2. siso controller

I

8

..

..

"'

...

Iii N 8 N

('\

/_]

\

,--- '\. 1 I /

'\)

O. IXJ '2.0 e.oo 111.0 24.0 TlHE S

"°·

0 '2.0

·

0

c. rotor speed d. electrical power

Fig. 2. Wind gust response of the wind turbine with the optimal output feedback controller (1) and with the siso controller (2)

·

6

Conclusions

For high performance electro-mechanical systems, a multivariable control system de-sign approach is motivated. The results for a wind energy conversion system as an example indicate that with a robust optimal output control system design superior per-formance can be obtained. This approach leads systematically to a proper compromise between power and speed fluctuations and mechanical loads. The design methodology is straightforward, and as simple as siso-controllers to implement in digital computer systems. The internal controller structure has been used as part of the design process,

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in order to obtain a more simple design. A multi- model extention of the method is given to obtain robustness with respect to non-linearities.

Acknowledgemenu

The reseach on the control system design for the wind energy conversion system re-ported in this paper, was carried out at the Automation Engineering Department, Division for Engineering and Consultancy, N.V.KEMA, Arnhem, The Netherlands, in co-operation with the Measurement and Control Group, Mechanical Engineering Department, Delft University of Technology, Delft, The Netherlands. The work was supported financially by the Dutch Electricity Generating Board (SEP).

References

Anderson, P.M., and F.F. Fouad (1982). Power aydem control and atability, vol.1.

Iowa State University Press, 3rd ed. Ames.

Anderson, B.D.O., and J.B. Moore (1971). Linear optimal control. Prentice-Hall, Englewood Cliffs, N .J.

Levine, W.S., and M. Athans (1970). On the determination of the optimal constant output feedback gains for linear multivariable systems, IEEE Trana. on Aut. Control,

15(1 ), pp.44-48.

Makila, P.M., and H.T. Toivonen (1987). Computational methods for parametric LQ problems -a survey. IEEE Trana. Aut. Control, ac-3.!, 8, pp.658-671.

Steinbuch, M. (1986). Dynamic modelling and analysis of a wind turbine with variable speed, Journal A, .!7(1), pp. 1-8.

Steinbuch, M. (1987). Optimal multivariable control of a wind turbine with variable speed, Wind Engineering, 11(3), pp.153- 163.

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