Figure 1.
(
a) Schematic diagram of a double-loop analog control system with the capacitor current feedback and an analog PWM modulator, (
b) continuous-time model with one reference input according to [
14,
17,
21,
22,
23].
is the ESR of the choke.
Figure 1.
(
a) Schematic diagram of a double-loop analog control system with the capacitor current feedback and an analog PWM modulator, (
b) continuous-time model with one reference input according to [
14,
17,
21,
22,
23].
is the ESR of the choke.
Figure 2.
Schematic diagrams of digital control systems: (a) 1Ld-digital single loop, (b) 2Ld-digital double loop. Switches symbolize sampling performed by Analog-to-Digital-Converters (ADC).
Figure 2.
Schematic diagrams of digital control systems: (a) 1Ld-digital single loop, (b) 2Ld-digital double loop. Switches symbolize sampling performed by Analog-to-Digital-Converters (ADC).
Figure 3.
Schematic diagrams of hybrid control systems: (a) single loop, 1Lh (b) double-loop, 2Lh. It is assumed that the continuous sine wave is produced from the discrete sinusoidal reference passed by a Digital-to-Analog-Converter (DAC) and an analog smoothing filter.
Figure 3.
Schematic diagrams of hybrid control systems: (a) single loop, 1Lh (b) double-loop, 2Lh. It is assumed that the continuous sine wave is produced from the discrete sinusoidal reference passed by a Digital-to-Analog-Converter (DAC) and an analog smoothing filter.
Figure 4.
(
a) Schematic diagram of the rectifier RC load, (
b) abruptly changing resistive load. According to [
7,
28,
29,
31], the parameters for th rectifier load in (
a) are
,
F,
. For the abruptly changing resistive load in (
b) there is
.
is periodically turned on when the reference sine wave
, and off when it reaches
or
.
Figure 4.
(
a) Schematic diagram of the rectifier RC load, (
b) abruptly changing resistive load. According to [
7,
28,
29,
31], the parameters for th rectifier load in (
a) are
,
F,
. For the abruptly changing resistive load in (
b) there is
.
is periodically turned on when the reference sine wave
, and off when it reaches
or
.
Figure 5.
(a) Poles and zero, (b) step responses, (c) Bode, and (d) Nyquist plots of the open-loop system in two modes. Blue lines—idle, green lines—activ load. In the no-load mode there is , . The resonant frequencies are Hz for , and Hz for . Note small differences between characteristics of the no-load and the resistive load system, and a large discrepancy between the no-load and RC load system.
Figure 5.
(a) Poles and zero, (b) step responses, (c) Bode, and (d) Nyquist plots of the open-loop system in two modes. Blue lines—idle, green lines—activ load. In the no-load mode there is , . The resonant frequencies are Hz for , and Hz for . Note small differences between characteristics of the no-load and the resistive load system, and a large discrepancy between the no-load and RC load system.
Figure 6.
Illustration of various modulation methods: (a)-PAM, (b)-PWM, (c)-PWM, (d)-PWM. Red crosses denote samples of the input signal, yellow dots-switching instants on the intersection of the modulating function with appropriate sampled value.
Figure 6.
Illustration of various modulation methods: (a)-PAM, (b)-PWM, (c)-PWM, (d)-PWM. Red crosses denote samples of the input signal, yellow dots-switching instants on the intersection of the modulating function with appropriate sampled value.
Figure 7.
(a) Open loop PWM controlled system model, and (b) QCT model of the system in (a).
Figure 7.
(a) Open loop PWM controlled system model, and (b) QCT model of the system in (a).
Figure 8.
Dependence of and THD from and M in the no-load open loop PWM and PWM controlled system. (a,b): ; , = 12.8, 25.6 and 51.2 kHz, (c,d): ; kHz, M = 0.2, 0.5, 0.8.
Figure 8.
Dependence of and THD from and M in the no-load open loop PWM and PWM controlled system. (a,b): ; , = 12.8, 25.6 and 51.2 kHz, (c,d): ; kHz, M = 0.2, 0.5, 0.8.
Figure 9.
Capacitor current
in the open-loop inverter of
Figure 7a using different modulation types compared with QCT output of the model of
Figure 7b and the sampled values. The plots in (
a) are for the no-load system and in (
b) for the inverter with a RC rectifier load. Observe that for PWM
and PWM
the sampled values and the QCT values overlap, and for PWM
they differ. Details are shown for individual sampling periods enlarged in the figures in (
b).
Figure 9.
Capacitor current
in the open-loop inverter of
Figure 7a using different modulation types compared with QCT output of the model of
Figure 7b and the sampled values. The plots in (
a) are for the no-load system and in (
b) for the inverter with a RC rectifier load. Observe that for PWM
and PWM
the sampled values and the QCT values overlap, and for PWM
they differ. Details are shown for individual sampling periods enlarged in the figures in (
b).
Figure 10.
Schematic diagrams of QCT models for digital control systems depicted in
Figure 3a: (
a) 1Ld-single loop and (
b) 2Ld-double-loop with the capacitor current feedback.
Figure 10.
Schematic diagrams of QCT models for digital control systems depicted in
Figure 3a: (
a) 1Ld-single loop and (
b) 2Ld-double-loop with the capacitor current feedback.
Figure 11.
Schematic diagrams of QCT models for hybrid control systems depicted in
Figure 2: (
a) 1Lh-single loop and (
b) 2Lh-double-loop with the capacitor current feedback.
Figure 11.
Schematic diagrams of QCT models for hybrid control systems depicted in
Figure 2: (
a) 1Lh-single loop and (
b) 2Lh-double-loop with the capacitor current feedback.
Figure 12.
Exemplary surfaces of THD as functions of parameters (a) THD() for 2Lh (P+P) and (b) THD(,) for 2Lh (PI+P), (c) zoomed in view of (b).
Figure 12.
Exemplary surfaces of THD as functions of parameters (a) THD() for 2Lh (P+P) and (b) THD(,) for 2Lh (PI+P), (c) zoomed in view of (b).
Figure 13.
Dependence of (a) the gain for PID single-loop controllers, (b) and (c) of PI+P double-loop structures as functions of carrier frequency in both digital and hybrid implementation.
Figure 13.
Dependence of (a) the gain for PID single-loop controllers, (b) and (c) of PI+P double-loop structures as functions of carrier frequency in both digital and hybrid implementation.
Figure 14.
Dependence of THD and the gain from the gain margin for different values carrier frequency : (a) 1Lh PID and (b) 1Ld PID.
Figure 14.
Dependence of THD and the gain from the gain margin for different values carrier frequency : (a) 1Lh PID and (b) 1Ld PID.
Figure 15.
Distortion function and THD values of in 1L (PD)/(PID) and 2L (P+P)/(PI+P) control systems optimized for rectifier RC load working at carrier frequencies 25.6 kHz; (a) (PD)/(P+P) controller and (b) (PID)/(PI+P) controller.
Figure 15.
Distortion function and THD values of in 1L (PD)/(PID) and 2L (P+P)/(PI+P) control systems optimized for rectifier RC load working at carrier frequencies 25.6 kHz; (a) (PD)/(P+P) controller and (b) (PID)/(PI+P) controller.
Figure 16.
THD
of
as a function of
H in optimally tuned control systems with
displayed in
Figure 15b. In (
a–
d) control structures are arranged as in
Figure 15b. Here
denotes the closed-loop resonant frequency in the no-load mode. According to Table 6, it equals approximately to 2.4 kHz for (
a), 2.9 kHz for (
b), 4.8 kHz for (
c) and 8.0 kHz for (
d).
Figure 16.
THD
of
as a function of
H in optimally tuned control systems with
displayed in
Figure 15b. In (
a–
d) control structures are arranged as in
Figure 15b. Here
denotes the closed-loop resonant frequency in the no-load mode. According to Table 6, it equals approximately to 2.4 kHz for (
a), 2.9 kHz for (
b), 4.8 kHz for (
c) and 8.0 kHz for (
d).
Figure 17.
Functions
and
and their sampled values in optimally tuned control systems ordered in (
a–
d) as in
Figure 16 at
= 25.6 kHz under a rectifier load. Note that the blurry shape of the continuous-time controller output
is due to large intersample deviations from the values at sampling instants
depicted in light blue.
Figure 17.
Functions
and
and their sampled values in optimally tuned control systems ordered in (
a–
d) as in
Figure 16 at
= 25.6 kHz under a rectifier load. Note that the blurry shape of the continuous-time controller output
is due to large intersample deviations from the values at sampling instants
depicted in light blue.
Figure 18.
Distortion function and THD values of in 1L (PID) and 2L (PI+P) control systems optimized for the RC rectifier load operating at different carrier frequencies : (a) 12.8 kHz, (b) 25.6 kHz, and (c) 51.2 kHz. All plots are displayed in the same scale. Plots in (a) extending beyond the display window are also displayed in the appropriate scale in Figure 25.
Figure 18.
Distortion function and THD values of in 1L (PID) and 2L (PI+P) control systems optimized for the RC rectifier load operating at different carrier frequencies : (a) 12.8 kHz, (b) 25.6 kHz, and (c) 51.2 kHz. All plots are displayed in the same scale. Plots in (a) extending beyond the display window are also displayed in the appropriate scale in Figure 25.
Figure 19.
Zoomed-in views of the distortion function
showed in
Figure 18c for various structures at carrier frequency
kHz.
Figure 19.
Zoomed-in views of the distortion function
showed in
Figure 18c for various structures at carrier frequency
kHz.
Figure 20.
THD values for different structures with controllers PI/PID and carrier frequencies . (a) THD in linear scale, (b,c) in logaritmic scale.
Figure 20.
THD values for different structures with controllers PI/PID and carrier frequencies . (a) THD in linear scale, (b,c) in logaritmic scale.
Figure 21.
Distortion function and THD values of in 1L (PID) and 2L (PI+P) control systems optimized for the rectifier resistive load operating at different carrier frequencies : (a) 12.8 kHz, (b) 25.6 kHz, and (c) 51.2 kHz. Plots in (a) extending beyond the display window are displayed in the appropriate scale in Figure 25.
Figure 21.
Distortion function and THD values of in 1L (PID) and 2L (PI+P) control systems optimized for the rectifier resistive load operating at different carrier frequencies : (a) 12.8 kHz, (b) 25.6 kHz, and (c) 51.2 kHz. Plots in (a) extending beyond the display window are displayed in the appropriate scale in Figure 25.
Figure 22.
Root loci of 1L PID hybrid and digital control systems for different values of . The top row is for 1Lh (PID), the (bottom) row for 1Ld (PID). From (left) to (right), takes ascending values of 12.8 kHz, 25.6 kHz, and 51.2 kHz. The dominant roots are indicated by arrows.
Figure 22.
Root loci of 1L PID hybrid and digital control systems for different values of . The top row is for 1Lh (PID), the (bottom) row for 1Ld (PID). From (left) to (right), takes ascending values of 12.8 kHz, 25.6 kHz, and 51.2 kHz. The dominant roots are indicated by arrows.
Figure 23.
Comparison of (a) 2Lh (PI+P) with (b) 1Lh (PID) and (c) 2Ld (PI+P) with (d) 1Ld (PID) at kHz. Comparison of hybrid and digital systems is also possible. The dominant roots are shown by arrows.
Figure 23.
Comparison of (a) 2Lh (PI+P) with (b) 1Lh (PID) and (c) 2Ld (PI+P) with (d) 1Ld (PID) at kHz. Comparison of hybrid and digital systems is also possible. The dominant roots are shown by arrows.
Figure 24.
Dominant roots of the closed-loop systems. (
a,
b) single-loop systems, (
c,(
d) double-loop systems. Axis scales other than in
Figure 22 and
Figure 23 are used to show the details. Therefore, angle
differs from
. In particular,
,
for
, and
,
for
.
Figure 24.
Dominant roots of the closed-loop systems. (
a,
b) single-loop systems, (
c,(
d) double-loop systems. Axis scales other than in
Figure 22 and
Figure 23 are used to show the details. Therefore, angle
differs from
. In particular,
,
for
, and
,
for
.
Figure 25.
Plots of , and for the rectifier RC load and abruptly changing resistive load in a 1Ld(PID) system at 12.8 kHz using PWM and PWM modulation. (a) PWM, rectifier load; (b) PWM, rectifier load; (c) PWM, resistive load; (d) PWM, resistive load. The presence of slow real root in the no-load mode demonstrates visually in the last part of the plots in (a,b), and in the first part of the plots for a system with a resistive load in (c,d), as asymmetry with respect to the time axis. Observe that there is greater agreement between PWM and QCT than between PWM and QCT.
Figure 25.
Plots of , and for the rectifier RC load and abruptly changing resistive load in a 1Ld(PID) system at 12.8 kHz using PWM and PWM modulation. (a) PWM, rectifier load; (b) PWM, rectifier load; (c) PWM, resistive load; (d) PWM, resistive load. The presence of slow real root in the no-load mode demonstrates visually in the last part of the plots in (a,b), and in the first part of the plots for a system with a resistive load in (c,d), as asymmetry with respect to the time axis. Observe that there is greater agreement between PWM and QCT than between PWM and QCT.
Figure 26.
Frequency plots
of the closed-loop systems. Collections of
for all structures considered at various carrier frequencies
: (
a) 12.8 kHz; (
b) 25.6 kHz; (
c) 51.2 kHz. The values of
are summarized in
Table 6.
Hz.
Figure 26.
Frequency plots
of the closed-loop systems. Collections of
for all structures considered at various carrier frequencies
: (
a) 12.8 kHz; (
b) 25.6 kHz; (
c) 51.2 kHz. The values of
are summarized in
Table 6.
Hz.
Figure 27.
and comparison of (a) 1L structures and (b) 2L structures at various .
Figure 27.
and comparison of (a) 1L structures and (b) 2L structures at various .
Figure 28.
Influence of PWM type on control. The capacitor current and distortion function are displayed for the structures (a) 1Ld (PID), (b) 2Ld (PI+P), (c) 1Lh (PID), and (d) 2Lh (PI+P) operating at 25.6 kHz.
Figure 28.
Influence of PWM type on control. The capacitor current and distortion function are displayed for the structures (a) 1Ld (PID), (b) 2Ld (PI+P), (c) 1Lh (PID), and (d) 2Lh (PI+P) operating at 25.6 kHz.
Figure 29.
Control in the OL system with rectifier RC load. (a–c) steady-state variables, (d) start-up process. Note that the start-up process is very fast.
Figure 29.
Control in the OL system with rectifier RC load. (a–c) steady-state variables, (d) start-up process. Note that the start-up process is very fast.
Figure 30.
Control with the digital P controller. (a–c) steady-state variables, (d) THD as a function of . Note a small improvement of THD from 3.72% in OL to 2.9% with the P controller.
Figure 30.
Control with the digital P controller. (a–c) steady-state variables, (d) THD as a function of . Note a small improvement of THD from 3.72% in OL to 2.9% with the P controller.
Figure 31.
(a) , (b) and (c) root locus of R controlled system in the no-load mode for various . As increases, oscillability at increases. The system loses stability at .
Figure 31.
(a) , (b) and (c) root locus of R controlled system in the no-load mode for various . As increases, oscillability at increases. The system loses stability at .
Figure 32.
R control at different values of gain . (a) , , no-load mode is stable; (b) , , no-load mode is stable; (c) , , no-load mode is stable but close the stability boarder; (d) , , no-load mode is unstable.
Figure 32.
R control at different values of gain . (a) , , no-load mode is stable; (b) , , no-load mode is stable; (c) , , no-load mode is stable but close the stability boarder; (d) , , no-load mode is unstable.
Figure 33.
Start-up process of the R control. (
a–
h) Transients of
ordered for increasing values of
. Note that it is slower than in OL in
Figure 29, even for large
.
Figure 33.
Start-up process of the R control. (
a–
h) Transients of
ordered for increasing values of
. Note that it is slower than in OL in
Figure 29, even for large
.
Figure 34.
Surfaces of THD values as functions of controller gains for (a) PI, (b) PR, and (c) IR control systems. Parameters leading to the lowest THD values are marked with a reddish background.
Figure 34.
Surfaces of THD values as functions of controller gains for (a) PI, (b) PR, and (c) IR control systems. Parameters leading to the lowest THD values are marked with a reddish background.
Table 1.
Values of the relative delay as functions of M and .
Table 1.
Values of the relative delay as functions of M and .
M | (kHz) | PAM | PWM | PWM | PWM |
---|
| 12.8 | 0.5000 | 0.0849 | 0.5000 | 0.5000 |
0.2 | 25.6 | 0.5000 | 0.0849 | 0.5000 | 0.5000 |
| 51.2 | 0.5000 | 0.0849 | 0.5000 | 0.5000 |
| 12.8 | 0.5000 | 0.2122 | 0.5000 | 0.5000 |
0.5 | 25.6 | 0.5000 | 0.2122 | 0.5000 | 0.5000 |
| 51.2 | 0.5000 | 0.2122 | 0.5000 | 0.5000 |
| 12.8 | 0.5000 | 0.3395 | 0.5000 | 0.5000 |
0.8 | 25.6 | 0.5000 | 0.3395 | 0.5000 | 0.5000 |
| 51.2 | 0.5000 | 0.3395 | 0.5000 | 0.5000 |
Table 2.
The values of THD for a no-load open-loop PWM-controlled system as a function of M and .
Table 2.
The values of THD for a no-load open-loop PWM-controlled system as a function of M and .
| PWM and PWM | PWM |
---|
| | |
---|
(kHz) | 0.2 | 0.5 | 0.8 | 0.2 | 0.5 | 0.8 |
---|
12.8 | 0.4263 | 0.3201 | 0.1913 | 0.4479 | 0.4693 | 0.5814 |
25.6 | 0.1063 | 0.0798 | 0.0477 | 0.1266 | 0.1892 | 0.2786 |
51.2 | 0.0266 | 0.0199 | 0.0119 | 0.0435 | 0.0881 | 0.1378 |
Table 3.
Values of the optimal gains , , for different systems, ().
Table 3.
Values of the optimal gains , , for different systems, ().
(kHz) | 1L (PD) | 2L (P+P) | 1L (PID) | 2L (PI+P) |
---|
digital | | | | |
12.8 | = 8.5 | = 8.4, = 0.20 | = 9.1 | = 8.1, = 0.22 |
25.6 | = 31.7 | = 15.5, = 0.50 | = 35.9 | = 17.2, = 0.45 |
51.2 | = 124.6 | = 30.4, = 1.01 | = 146.9 | = 37.2, = 0.80 |
hybrid | | | | |
12.8 | = 19.1 | = 23.3, = 0.78 | = 20.3 | = 23.3, = 0.72 |
25.6 | = 73.8 | = 46.5, = 1.55 | = 90.1 | = 46.5, = 1.45 |
51.2 | = 294.9 | = 93.1, = 3.08 | = 379.1 | = 93.1, = 2.95 |
Table 4.
Summary of THD values for the PWM modulator and QCT method, written as PWM/QCT, for the RC rectifier load. The difference between both components is due mainly to the ripple caused by the carrier signal.
Table 4.
Summary of THD values for the PWM modulator and QCT method, written as PWM/QCT, for the RC rectifier load. The difference between both components is due mainly to the ripple caused by the carrier signal.
(kHz) | 1L (PD) | 2L (P+P) | 1L (PID) | 2L (PI+P) |
---|
digital: | | | | |
12.8 | 2.011/1.980 | 1.753/1.469 | 2.156/2.141 | 1.782/1.559 |
25.6 | 0.793/0.786 | 0.548/0.506 | 0.717/0.717 | 0.419/0.409 |
51.2 | 0.239/0.238 | 0.150/0.144 | 0.184/0.183 | 0.083/0.081 |
hybrid: | | | | |
12.8 | 0.848/0.672 | 0.534/0.242 | 0.715/0.614 | 0.387/0.176 |
25.6 | 0.241/0.202 | 0.121/0.064 | 0.150/0.124 | 0.089/0.036 |
51.2 | 0.063/0.054 | 0.028/0.016 | 0.032/0.024 | 0.021/0.007 |
Table 5.
Dominant roots in various control structures and their parameters: , , and .
Table 5.
Dominant roots in various control structures and their parameters: , , and .
(kHz) | 1Ld (PID) | 2Ld (PI+P) | 1Lh (PID) | 2Lh (PI+P) |
---|
(Hz) |
12.8 | 1470 | 1714 | 2447 | 3929 |
25.6 | 2396 | 2930 | 4770 | 8018 |
51.2 | 4798 | 5938 | 9650 | 16,533 |
and |
12.8 | | | n.a. | n.a. |
| | ) | | |
25.6 | | | | |
51.2 | ) | | | |
Table 6.
Resonant frequencies for different structures and carrier frequencies .
Table 6.
Resonant frequencies for different structures and carrier frequencies .
(kHz) | 1Ld (PID) | 2Ld (PI+P) | 1Lh (PID) | 2Lh (PI+P) |
---|
(Hz) |
---|
12.8 | 1479 | 1714 | 2446 | 3930 |
25.6 | 2395 | 2927 | 4770 | 8013 |
51.2 | 4795 | 5922 | 9650 | 16,520 |