Min Parameter Variations
Min Parameter Variations
ABSTRACT Multi-converter electronic systems are becoming widely used in many industrial applications;
therefore, the stability of the whole system is a big concern to the real-world power supplies applications.
A multi-converter system comprised of cascaded converters has a basic configuration that consists of
two or more converters in series connection, where the first is a source converter that maintains a regulated dc
voltage on the intermediate bus while remaining are load converters that convert the intermediate bus voltage
to the tightly regulated outputs for the next system stage or load. Instability in cascaded systems may occur
due to the constant power load (CPL), which is a behavior of the tightly regulated converters. CPLs exhibit
incremental negative resistance behavior causing a high risk of instability in interconnected converters.
In addition, there are other problems apart from the CPL, e.g., non-linearities due to the inductive element
and uncertainties due to the imprecision of a mathematical model of dc–dc converters. Aiming to effectively
mitigate oscillations effects in the output of source converter loaded with a CPL, in this paper, an interval
robust controller, by linear programming based on Kharitonov rectangle, is proposed to regulate the output
of source converter. Several tests were developed by using an experimental plant and simulation models
when the multi-converter buck–buck system is subjected to a variation of power reference. Both simulation
and experimental results show the effectiveness of the proposed controller. Furthermore, the performance
indices computed from the experimental data show that the proposed controller outperforms a classical
control technique.
INDEX TERMS Constant power load (CPL), multi-converter buck-buck system, parametric uncertainties,
robust control based on Kharitonov rectangle, mitigation oscillations in multi-converter buck-buck system.
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K. E. Lucas Marcillo et al.: Interval Robust Controller to Minimize Oscillations Effects
power characteristic. Because of switching, the convert- In research on dynamic systems with parametric uncertain-
ers have some inherent nonlinear behaviors, e.g., high fre- ties, the techniques that deal with this problem have been
quency of switching, increasing harmonics in the system, studied extensively over the last 40 years [42], [43].
current and voltage distortion, and instabilities occur due this To the best of the authors’ knowledge, it seems that most
effects [12], [13]. Therefore, it is a challenging task to ensure papers published so far focus on mitigating the destabilizing
the stability, transient performance and higher efficiency of effect of CPL without considering the uncertainties present
such converters [13]. in the system parameters. Therefore, studies reporting robust
A multi-converter system comprised of cascaded convert- parametric methodologies for DC-DC converters feeding a
ers has a basic configuration that consists of two converters CPL to mitigate oscillations effects caused by CPL still
in series connection, where the first is a source converter scarce in literature. However, in [39], a novel multivariable
while the second one is a load converter. The source converter robust parametric technique was used for minimizing cou-
maintains a regulated DC voltage on the intermediate bus, and pling effect in single inductor multiple output DC-DC con-
the load converter transforms the intermediate bus voltage to verter operating in continuous conduction mode. Moreover,
tightly regulated outputs for the next system stage or load. In a in [40] and [41], the use of Robust Parametric Control (RPC)
cascaded buck converter system a large variety of dynamic techniques is proposed to stabilize oscillations at the output
and static interactions are possible and these can lead to of a buck converter caused by parametric uncertainties.
irregular behavior of a converter, a group of converters or the Recently, the study developed in [44] addressed the impor-
whole system. tant problem of parametric uncertainties in DC-DC convert-
When a converter tightly regulates its output, it behaves as ers by using µ analysis. However, their approach is focused
a Constant Power Load (CPL), thereby, in cascaded systems, only on a posterior analysis of system stability. The important
load converter acts as a CPL when it is tightly regulated, subject of robust controller synthesis has been not addressed.
its dynamic response is faster than the dynamic response of In contrast, this paper is focused in the problem of robust con-
the source converter and its switching operation frequency troller synthesis, being thoroughly addressed from the onset,
is faster than source converter [14]. If the source converter providing a practical and simple robust controller design
is faster than the load converter, then it will compensate for algorithm with sufficient level of the detail in order to be
disturbances and will regulate its output before the feedback easily implemented.
loop of the load converter reacts to disturbances. Therefore, In this context, this paper proposes a robust controller
the load converter will not act as a perfect CPL for the feeding based on RPC theory. The proposed controller is applied to
converter [15]–[21]. source converter in order to mitigate oscillations effects due to
Different from a resistive load, CPL is a nonlinear load CPL in multi-converter buck-buck (MCBB) system, aiming
with variable negative impedance characteristics, i.e., the to reduce the control effort when the system is submitted to
input current increases/decreases with a decrease/increase variation of power reference.
in its terminal voltage [15]–[21]. Because of the negative The main contributions of this work are briefly summa-
impedance characteristics of CPL, the system may become rized in that following:
unstable, which may lead the system into oscillation or fail- • By using the proposed robust technique, structured
ure, and stress or damage the system equipment when feed- uncertainties of the type hyperbox, considering interval
ing a CPL [17]–[21]. For this issue, CPLs are receiving parametric type, are taking into account from the outset
more attention of researchers to give solutions aiming to in the controller design process, incorporating available
cancel or compensate the negative effects of CPL. information about components (resistors, inductors, and
Traditionally, the stability analysis and controller design capacitors) tolerances or defined by designer.
of cascaded DC-DC converters is carried out by using the • The proposed robust technique leads to easy-to-
impedance criterion applied to averaged and linearized mod- implement controllers having fixed low-order structure,
els [19]–[22]. The load converter under a tight control is allowing the deployment of standard industry structures
conventionally modeled CPL for stability analysis or for such as PID and Lead-Lag.
controller design [19]–[22]. • Aiming to evaluate the performance of the proposed
In order to mitigate the destabilizing effect of CPL, several robust methodology under the instability problem
methods have been proposed [23], such as passive and active caused by a CPL, the proposed robust methodology
damping [24]–[26], Lyapunov redesign control [8], nonlin- is compared with classical methodology carrying out
ear feedback linearization [27]–[29], Sliding Mode Control several experimental and simulation tests. The perfor-
(SMC) [30]–[32], fuzzy control [33], Model Predictive Con- mance index (ISE) is computed to analyze the con-
trol (MPC) [34], [35] and robust control [36], [37]. However, trol methodologies compared in this work. The results
there are other problems apart from the CPL, e.g., uncer- show the proposed methodology outperforms the other
tainties present in the system parameters, which may lead approach.
to performance degradation [38]. In literature can be found The remainder of this paper is organized as follows.
control strategies applied to DC-DC power converters that Section II presents a brief review about the multi-converter
deal with parametric uncertainties [39]–[41]. buck-buck system; Section III presents a brief review about
operating duty cycle of load converter; and Po is the operating diL rL 1
1 = − 1 iL1 + −vc1
power of CPL. dt L1 L1 d1 Ts1 < t < Ts1
dvc1 1 1 vc1 Po
In order to maintain a constant power level, in a DC-DC
= iL1 − + ,
dt C1 C1 RL1 vc1
converter when it acts as a CPL, input current increases
when input voltage decreases, and vice versa, thus, the prod- (3)
uct of the input current and input voltage of the load con-
where d1 and Ts1 are the duty cycle and switching period of
verter, (i.e., Po = iinL vc1 ) is a constant. The instantaneous
the source converter, respectively. L1 , rL1 , C1 and RL1 are the
value of the load impedance is positive (i.e., vc1 /iinL > 0).
plant parameter of source converter. Vi is the input DC voltage
However, the incremental impedance is always negative
of source converter. Po is the output power of load converter
(i.e., 1vc1 /1iinL < 0) due to once appearing any distur-
that is constant. iouts = iL1 .
bance, thus operating point will leave from previous point
Using the state-space averaging method [14], [20],
and never return. This negative incremental impedance has a
the buck converter dynamics can be written as:
negative impact on the power quality and stability of system.
Fig. 4 shows the negative incremental impedance behavior diL rL 1
1 = − 1 iL1 + Vi d1 − vc1
of CPL. dt L1 L1
dvc1 1 1 vc1 Po
(4)
= iL1 − +
dt C1 C1 RL1 vc1
where, V̄i , d̄1 , VC1 and IL1 are the average values of Vi , d1 , vc1
and iL1 , respectively.
Substituting (5) in (4) and neglecting the internal resistance
of the inductor to simplify the calculations, the buck converter
model becomes
FIGURE 4. The negative incremental impedance behavior of CPL.
d ĩ
dtL1 = L1 V̄i d̃1 + d̄1 Vi − ṽc1
1
d ṽc1 P ṽ
(6)
1
dt = C ĩL1 − Vo 2c1
1 c1
B. STABILITY ANALYSIS OF STUDIED SYSTEM
The system, showed in Fig. 2(b), is used to show the insta- Note that the following approximation was made in (6),
bility of a DC-DC converter feeding a CPL. To obtain the V̄i Ṽi and Vc1 ṽc1 .
large-signal behavior of the load converter, the CPL is rep- Therefore, the transfer function of the buck converter
resented by a dependent current source [14], iCPL = Po /vc1 , loaded with a CPL can be obtained from (6) as follows:
so the instantaneous current drawn from source converter is d̄1
given by ṽc1 L1 C1
G(s) = = (7)
Ṽi Po 1
iouts (t) = iRL1 (t) + iCPL (t) s2 − C1 Vc2
s+ L1 C1
1
vc (t) Po
iouts (t) = 1 + Due to CPL, the transfer function in (7) have poles in the
RL1 vc1 (t)
right half-plane, thus, the buck converter, when it is loaded
iouts = iL1 (1)
with a CPL, is unstable.
Depending on switching of the source converter, the large- In (4), the nonlinear coefficient introduced by a CPL and
signal model of the converter in continuous conduction mode the constraints on the state variables make the equation diffi-
can be obtained based on the following equations: cult to solve. Therefore, any unwanted dynamics introduced
in (4) cannot be damped, so trajectories will tend to have
diL rL 1 cycling or unbounded behaviors [20], [21].
1 = − 1 iL1 + Vi − vc1
dt L1 L1 0 < t < d1 Ts1 The simulation results in Fig. 5 confirm the intuitive
dvc1 1 1 vc1 Po behavior suggested by (4).
= iL1 − + ,
dt C1 C1 RL1 vc1
The system is analyzed by a phase-plane analysis,
(2) solving (plotting) the system differential equations giving
as shown in (8) [38]. designed according to Keel and Bhattacharyya [45], associ-
m ated with a linear goal programming formulation, which will
bi , bi s
P − + i
lead to a set of linear inequality constraints.
B(s, b) i=0 Consider G(s, p) a uncertain plant of order n and C(s, x) the
G(s, b, a) = = n (8)
A(s, a) controller of order r, defined in (13) and (14) respectively.
ai , ai s
P − + i
i=0 n(s) b1 sn−1 + · · · + bn−1 s + bn
G(s, p) = = n (13)
Many robust stability tests under parametric uncertainty d(s) s + a1 sn−1 + · · · + an−1 s + an
are based on analysis of uncertain characteristic polynomial nc (s) x0 sr + x1 sr−1 + · · · + xr−1 s + xr
assumed as an interval polynomial family [38], such as C(s, x) = = r (14)
dc (s) s + y1 sr−1 + · · · + yr−1 s + yr
n
X Let p be the vector of parameters that represent the plant
pi , pi s
− + i
P(s, p) = (9) and x the vector of real parameters representing the controller
i=0
defined in (15) and (16) respectively. In addition, po rep-
Polynomial P(s, p) is stable if and only if all its roots are resents the nominal value of plant parameters defined in a
contained on the Left Half-Plane (LHP) of the s-plane. Then, hyperbox region of uncertainties.
P(s, p) is robustly stable if and only if all its polynomials
p := [ b1 b2 · · · bn−1 bn a1 a2 · · · an−1 an ] (15)
are stable for a set of operating point different from the
nominal operating point within its minimum and maximum p := [ x0 x1 · · · xr−1 xr y1 y2 · · · yr−1 yr ] (16)
limits [46]. However, it is not necessary to check stability According to [45], the solution of the Diophantine equa-
of an infinite number of polynomials to guarantee the robust tion (17) summarizes the pole-placement problem
stability. Robust stability can be checked through the analysis
of four polynomials within P(s, a); these polynomials can be d(s) = d(s)dc (s) + n(s)nc (s) (17)
found by Kharitonov Theorem [38], [47]. where, d(s) is the closed-loop characteristic polynomial.
Therefore, the parameters of the closed-loop characteristic
B. KHARITONOV STABILITY THEOREM polynomial are represented as follows:
The Kharitonov Theorem is a test used in robust control
theory to evaluate the stability of a dynamic system whose di = di (x, p) (18)
parameters vary within a closed real interval as follows: Assuming that the desired dynamic of closed-loop system
δ(s) = δ0 + δ1 s + δ2 s + δ3 s + · · · + δn s
2 3 n
(10) is represented by
1d (s) = si + φ1 si−1 + · · · + φi−1 s + φi (19)
where, the coefficient vector δ̄ = [δ0 , δ1 , δ2 , δ3 , · · · , δn ]
ranges over a box: where, φi represent the parameters of the closed-loop desired
polynomial.
1 = δ0− , δ0+ × δ1− , δ1+ × · · · × δn− , δn+
(11) In order to tune the controller, the closed-loop polynomial
parameters are compared with the desired closed-loop poly-
where, δn− and δn+ represent the lower and upper limit respec-
nomial, which represent the desired dynamics of the system
tively. Therefore, the Kharitonov polynomials are defined as:
follow as
K1 (s) = δ0− +δ1− s+δ2+ s2 +δ3+ s3 +δ4− s4 +δ5− s5 +δ6+ s6 +· · · di (x, po ) = φi , i = 1, 2, . . . , l (20)
K2 (s) = δ0− +δ1+ s+δ2+ s2 +δ3− s3 +δ4− s4 +δ5+ s5 +δ6+ s6 +· · ·
This problem can be written in its matrix format, presenting
K3 (s) = δ0+ +δ1− s+δ2− s2 +δ3+ s3 +δ4+ s4 +δ5− s5 +δ6− s6 +· · · the following relationship [38], (21), as shown at the bottom
K4 (s) = δ0+ +δ1+ s+δ2− s2 +δ3− s3 +δ4+ s4 +δ5+ s5 +δ6− s6 +· · · of the next page.
(12) When the system is subject to parametric uncertain-
ties, the controller performance may deteriorate. Therefore,
Theorem 1 (Robust Stability): The interval polynomial the controller must guarantee robust performance within an
family delimited by 1 is robustly stable if and only if its acceptable region of closed-loop parameters variation, so that
four Kharitonov polynomials are stable [38], [47], i.e., all the closed-loop poles are located in a certain region. Thereby,
roots of the interval polynomial are in the SPL of the complex a desired region is defined as follows:
plane [48].
8 := φi− ≤ φi ≤ φi+
(22)
C. ROBUST CONTROLLER DESIGN BY Therefore, according to [46], replacing the parameters of
INTERVAL POLE-PLACEMENT (22) in (20), it is possible to formulate a linear inequalities
To design the controller, a region of uncertainty is previously set, which restricted the controller and desired polynomial
defined, considering that the uncertainty is contained in the coefficients in the predefined intervals, as shown in (23).
parameter variation of the plant-model. The controller is Thus, the closed-loop system has its poles within the roots
X = arg (minf (X ))
B(φ + )
A(p)
s.t. X≤ (24)
−A(p) −B(φ − )
FIGURE 7. Multi-Converter Buck-Buck System.
where, f (X ) is a linear cost function that must be built
and minimized according to the control goals. In this study,
the cost function f (X ) has been chosen to be the sum
respective equivalent circuits.
of the elements of vector of the controller parameter X ,
such as suggested by Keel and Bhattacharyya [45] and
diL
Bhattacharyya et al. [50].
L1 1 = d1 Vi − VC1 − rL1 iL1
dt
dV VC1
C1
IV. MATHEMATICAL MODEL FOR MULTI-CONVERTER C1 dt = iL1 − R
L1
BUCK-BUCK SYSTEM (25)
diL
In order to represent the dynamical behavior of DC Multi-
L2 2 = d2 VC1 − VC2 − rL2 iL2
converter buck-buck System, a small signal approximation
dt
model is employed as an effective mathematical model.
dV C2 VC
C2 = iL2 − 2
Fig. 7 represents the DC MCBB system with two decou- dt RL2
pled outputs, VC1 and VC2 , such that VC2 < VC1 , and a topol-
ogy employed to control the system. The main characteristic The duty cycle d1 regulates the output voltage (VC1 )
of this system is that it has two DC-DC buck converters of source converter, i.e. the DC bus voltage, and the duty
connected in series where the output of the first one converter cycle d2 regulates the output power of load converter,
is the DC source of the second one. i.e., VC2 2 /RL2 . Thereby, the outputs of system are described
Each converter can be considered an independent sub- below.
system; therefore, the dynamics of the system can be sim-
y1 = 0 VC1
plified to the analysis of two independent converters. The h i
2
dynamic behavior of buck converter, in Continuous Conduc- y2 = 0 VRC2 (26)
L2
tion Mode (CCM), can be found in [40] and [41].
The following equations involving the state variables of Assuming that the electronic switches and diodes are ideal,
buck converters are written based on the analysis of their the linearized model that describes the dynamic behavior of
[b1 ] 0
··· 0 0 | 1 0 ··· 0 0
x0
.. .. .. ..
. . . .
x
[b2 ] [b1 ] 0 | [a1 ] 1 0 1
.. .. .. .. .. .. ..
[φ1 ] − [a1 ]
. [b2 ] . 0 . | . [a1 ] . 0 .
.
[φ2 ] − [a2 ]
.. . .. .. xr−1
. ..
. . [b1 ] . .
[bm−1 ] 0 | [an−1 ] 1 0 .
x r
. ..
[bm ] [bm−1 ] . . [b2 ]
. [a1 ] − = [φ ] − [a ] (21)
[b1 ] | [an ] [an−1 ] 1 n n
. . .. .. y [φ ]
0
.. .. n+1
.
0 0 . ..
[bm ] [b2 ] | [an ] [a1 ]
y1
.
. . .. .. .. ..
.. . ..
. [bm−1 ] . . . [an−1 ] .
.
0 | 0 [φm ]
. ..
.. . . . [b ] [b ..
y
. . [an ] [an−1 ]
0 r−1
| {z }
m m−1 ] | 0
B
0 0 ··· 0 [bm ] | 0 0 ··· 0 [an ] yr
| {z } | {z }
X
A
the converter is represented as follows: step 1, by defining the nominal plant (20) with its operating
d1o conditions; in step 2, the box region of uncertainties is built
VC1 (s) L1 C1 based on a previously specified uncertainty range delimited
= rL
rL1
(27)
Vi (s) s2 + RL 1C1 + L11 s + L11C1 + by the designer. Since box region of uncertainties influence
RL1 L1 C1
1
o q on the delimitation of the convex region where the control
d2 Po
2 gains will be determined, the correct selection of this box
VC2 (s) L1 C1 RL2
= rL
rL2
(28) region is an important point to have success of the proposed
VC1 (s) s2 + RL 1C2 + L22 s + L21C2 + methodology. The lower-and upper-bound of each parameter
2
RL2 L2 C2
are provided in Table 1.
where, d1o
and d2o
are operational point for duty cycle of The characteristic closed-loop polynomial is obtained
outputs 1 and 2, respectively. Po is the operating power of (Step 3) by using the controller parameter and the nominal
output 2. model (20) selected in step 1, then by replacing the nominal
The nominal values of the parameters, operational point and interval values, defined in step 2, the interval closed-loop
and the meaning of each symbol in (27) and (28) are presented polynomial is calculated.
in Table 1. The controller function depends on the chosen control
structure. In this work, a controller with a PID structure is
TABLE 1. Values for the physical parameters of the DC multi-converter
buck-buck board test system. selected. The transfer function is given below.
U (s) kd s2 + kp s + ki
CPID (s) = = (29)
E(s) s
For simplification, transfer function presented in (20) can
be represented as follows:
VC1 (s) b0
G1 (s) = = 2 (30)
Vi (s) s + a1 s + a0
where
1 rL
a1 = + 1 (31)
RL1 C1 L1
1 rL1
a0 = + (32)
L1 C 1 RL1 L1 C1
do
b0 = 1 (33)
L1 C1
Finally, closed-loop interval polynomial is obtained by
using the controller parameters (22) and plant
parameters (23).
Pcl (s) = s3 + ϕ2− , ϕ2+ s2 + ϕ1− , ϕ1+ s + ϕo− , ϕo+
(34)
The nominal parameters of Pcl depend on the parameters
of source converter (cf. Table 1), resulting in the following
V. ROBUST CONTROLLER DESIGN METHODOLOGY nominal parameters:
This section presents a method to design a fixed order robust
controller that provides robust stability and performance for ϕ0o = b0 ki (35)
a predetermined uncertain family of models with parame- ϕ1o = a0 + b0 kp (36)
ters bounded in a hyperbox region. This study only con- ϕ2o = a1 + b0 kd (37)
siders uncertainties in the parameters of source converter
The lower- and upper-limits for these parameters must be
(see Table 1) because oscillations, caused by a CPL, occur
computed by replacing the nominal and interval presented
in the LC filter of the converter. Therefore, only output 1 will
in Table 1 by using interval analysis for (23)-(26). The region
be regulated by a robust controller. A classic controller, based
defined by the closed-loop interval polynomial of (27) must
on Classical Pole-Placement (CPP), will regulate output 2.
be inside the region determined by the desired performance
The robust controller is designed according to presented
polynomial (chosen in Step 4). Particularly, it was chosen for
by Bhattacharyya et al. [50]. In this paper, this method is
a maximum settling time of less than 0.15 sec and a damping
denominated as ‘‘Control Based on Kharitonov’s Rectangle
factor greater than 0.9, defining the desired performance
(CKR’’. The proposed controller must ensure robust stability
region (38). Note that an auxiliary pole must be added that
and performance for the entire region of parametric variation.
does not affect the desired dynamics of system to satisfy (20).
Fig. 8 illustrates a simplified flowchart of the methodology
for designing the robust controller. The process starts in 8 = s3 + [φ2 ] s2 + [φ1 ] s + [φo ] (38)
h0 z2 + h1 z + h2
CPID (z) = (39)
z2 − 1
FIGURE 17. The cost function ISE of system outputs for positive variations
of power reference. (a) Simulation assessment. (b) Experimental
FIGURE 19. The control effort test of experimental system, when the
assessment.
system is subjected to positive variations on the value of power reference.
FIGURE 20. The cost function ISE of effort control system for positive
variations of power reference. (a) Simulation assessment.
FIGURE 18. The control effort test of simulated system, when the system (b) Experimental assessment.
is subjected to positive variations on the value of power reference.
controller by CKR method as shown by the ISE performance For the simulated case, the control effort obtained was
indices in Figs. 17(a) and 17(b), ratifying the robustness of almost similar for controllers of system as shown their ISE
the proposed methodology. performance indices in Fig. 20(a). However, the performance
Figs. 18 and 19 show the control effort of controllers for presented by controllers in experimental tests was different as
simulated and experimental tests, respectively, using a PID shown in Fig. 20(b).
control structures. The DC multi-converter buck-buck system obtained
Note that the saturation of the control signal does not occur less degradation in the control system performance when
at any time. the robust proposed controller controls the output 1 of
FIGURE 28. The control effort test of simulated system, when the system
FIGURE 27. The cost function ISE of system outputs for negative is subjected to negative variations on the value of power reference.
variations of power reference. (a) Simulation assessment.
(b) Experimental assessment.
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