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Cascade-loop control design for
400Hz Ground Power Unit
Tran Que Son, Dong Pham Van, Hung Nguyen Dinh
Bao, Nguyen Quang Dich, and Nguyen Kien Trung
OUTLINE
• Introduction
1
• GPU model
2
• Control System Design
3
• A case study
4
• Conclusion
5
9/5/2022 2
GPU OVERVIEW
9/5/2022 3
3
Ground power unit (GPU) is a 400 Hz
voltage source inverter supplying the
airplanes with external electric power
during stopovers.
Reduce the noise, air pollution.
The standard rating of GPU:
 115V RMS, 400-Hz with three phase four
wires
 Power rating: 90 kVA (up to 180 kVA in
1s after starting)
Introduction GPU model
Control System
Design
A case study Conclusion
9/5/2022 4
Figure 1: Proposed GPU configuration
Improve system reliability in working with unbalanced loads
Reduce system volume, size and cost
Introduction GPU model
Control System
Design
A case study Conclusion
INVERTER TOPOLOGY
GPU TRANSFER FUNCTION
The PWM function is as follows:
𝐺𝑃𝑊𝑀 =
1
1.5𝑇𝑠𝑠+1
(3)
9/5/2022 5
Introduction GPU model
Control System
Design
A case study Conclusion
The state space equation of LC circuit:
𝑑𝑖𝐿
𝑑𝑡
𝑑𝑣𝑂
𝑑𝑡
=
−𝑟
𝐿
−1
𝐿
1
𝐶
0
𝑖𝐿
𝑣0
+
1
𝐿
0
0
−1
𝐶
𝑣𝐼
𝑖𝑂
(1)
GPU model can be written:
𝑣𝑂 =
𝑣𝐼
𝐿𝐶𝑠2+𝑟𝐶𝑠+1
−
(𝑠𝐿+𝑟)𝑖𝑂
𝐿𝐶𝑠2+𝑟𝐶𝑠+1
(2)
If consider 𝑖𝑂 are disturbance, the GPU transfer function will be:
𝐺 =
1
𝑁(1.5𝑇𝑠𝑠+1)(𝐿𝐶𝑠2+𝑟𝐶𝑠+1)
(4)
9/5/2022 6
OVERALL CONTROL SYSTEM
Introduction GPU model
Control System
Design
A case study Conclusion
Under the consideration that coupling components is not
significantly, can be ignored. Voltage and current loop control have
no effect each other, can be designed separately.
Figure 2: Overall control system diagram
9/5/2022 7
DEADBEAT CURRENT LOOP CONTROL DESIGN
Introduction GPU model
Control System
Design
A case study Conclusion
Figure 3: DB current
loop
Then, the DB controller function is:
𝑅𝑖 𝑧 = 𝑟𝐿
1−𝑒
−𝑟𝐿
𝐿
𝑇𝑠
1−𝑒
−𝑟𝐿
𝐿
𝑇𝑠𝑧−1
1−𝑧−2 (7)
The current loop transfer function,
can be derived:
𝐻𝑖 𝑧 =
𝑖𝐿
𝑖𝑟𝑒𝑓
= 𝑧−2
(5)
The current plant model 𝐺𝑖(𝑧) is determined by [8]:
𝐺𝑖 𝑧 =
1−𝑒
−𝑟𝐿
𝐿
𝑇𝑠
𝑟𝐿
𝑧−1
1−𝑒
−𝑟𝐿
𝐿
𝑇𝑠
𝑧−1
(6)
9/5/2022 8
Figure 4: Discrete parallel resonant voltage controller
[2] F. Rojas, R. Cardenas, J. Clare, M. Diaz, J. Pereda and R. Kennel: A Design Methodology of Multiresonant Controllers for High Performance 400 Hz
Ground Power Units. IEEE Transactions on Industrial Electronics, vol. 66, no. 8, pp. 6549-6559, Aug. 2019.
VOLTAGE RESONANT CONTROL DESIGN
The s domain resonant controller transfer function can be written as [3]:
𝑅𝑛(𝑠) = 𝐾𝑟𝑛
𝑠𝑐𝑜𝑠 𝜃𝑛 −𝜔𝑛𝑠𝑖𝑛 𝜃𝑛
𝑠2−𝜔𝑛
2 (8)
In which, 𝐾𝑟𝑛 is the gain and 𝜃𝑛 is the resonance frequency for the nth
resonant compensator
Introduction GPU model
Control System
Design
A case study Conclusion
9/5/2022 9
[3] Z. Li, Y. Li, P. Wang, H. Zhu, C. Liu and F. Gao: Single-Loop Digital Control of High-Power 400-Hz Ground Power Unit
for Airplanes. IEEE Transactions on Industrial Electronics, vol. 57, no. 2, pp. 532-543, Feb. 2010.
DISCRETE RESONANT CONTROLLER
By Zero Order Hold (ZOH) transform, the model of resonant controller in the
discrete domain can be obtained [3]:
𝑅𝑧(𝑛) =
𝑧−1 𝑠𝑖𝑛 𝜔𝑛𝑇𝑆 𝑐𝑜𝑠 𝜃𝑛 −(𝑧+1) 1−cos(𝜔𝑛𝑇𝑆) 𝑠𝑖𝑛 𝜃𝑛
𝑧2−2 cos 𝜔𝑛𝑇𝑆 𝑧+1 𝜔𝑛
(9)
With 𝑇𝑆 is the system sampling period.
Introduction GPU model
Resonant
controller
A case study Conclusion
9/5/2022 10
10
Introduction GPU model
Control System
Design
A case study Conclusion
SYSTEM PARAMETERS
The system parameters are listed in the Table 1.
PARAMETERS VALUE
Induction L = 200 µH
Capacitance C = 25 µF
Inductor resistance 0.02 
Switching frequency fc = 18 kHz
Output voltage 115V, 400 Hz
Transformer ration 5/3
Table 1: System parameters
9/5/2022 11
11
Introduction Inverter topology
Control system
design
A case study Conclusion
MATLAB SIMULATION
THD = 0.97%
Figure 5: Resistive load R = 1.09 with fundamental controller only
The case of linear load R = 1.09,
only fundamental controller is
required.
9/5/2022 12
12
Introduction Inverter topology
Control system
design
A case study Conclusion
MATLAB SIMULATION
Figure 6: Output voltage with a) only fundamental controller b) with 3rd controller is added
THD = 2.26%
THD = 1.9%
The case of nonlinear load, included a diode rectifier, a capacitor of 50µF and a load 1.09 Ω
9/5/2022 13
13
Introduction Inverter topology
Control system
design
A case study Conclusion
MATLAB SIMULATION
Figure 7: In the case of a sudden load change a) With DB settling time is 0.035s b) Without DB is 0.08s
Figure 5: Output voltage without DB current controller
THD = 2.39%
9/5/2022 14
14
Introduction Inverter topology
Control system
design
A case study Conclusion
EXPERIMENT SYSTEM DESIGN
Figure 8: Experiment system
A 90 kVA GPU prototype based on Texas Instrument TMS320F28379D
microcontroller was built verify the proposed design method
9/5/2022 15
15
Introduction Inverter topology
Control system
design
A case study Conclusion
EXPERIMENT RESULTS
Figure 9: Nonlinear load condition with fundamental controller only
The case of nonlinear load, only fundamental controller is implemented:
THD = 3.29%
9/5/2022 16
16
Introduction Inverter topology
Control system
design
A case study Conclusion
EXPERIMENT RESULTS
Figure 10: Output voltage under nonlinear load condition with 3rd compensator is added
With 3rd compensator is added
THD = 2.93%
3rd harmonic = 1.9%
9/5/2022 17
17
 A improvement for GPU configuration is proposed enhance the system
reliability under unbalanced load conditions, also reduce the volume, size and
production cost.
 Parallel resonant controller is applied in voltage control loop to control the
fundamental voltage also compensate the harmonics.
 Deadbeat control algorithm is implemented for inner current loop to remain
inductor current stable, contributing to the harmonic distortion compensation
at the output voltage
 Simulation and experiment results indicate that proposed system can produce a
good quality voltage even under the nonlinear load conditions.
 Higher order harmonic compensators (5th, 7th) will be next applied to control
system to improve the system performance.
Introduction Inverter topology
Control system
design
A case study Conclusion
CONCLUSION
9/5/2022 18
Thank you for attending!
Presenter: Tran Que Son
Email: tranqueson.ktdt@tnut.edu.vn

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ICERA2021_Present_Final.pptx

  • 1. Cascade-loop control design for 400Hz Ground Power Unit Tran Que Son, Dong Pham Van, Hung Nguyen Dinh Bao, Nguyen Quang Dich, and Nguyen Kien Trung
  • 2. OUTLINE • Introduction 1 • GPU model 2 • Control System Design 3 • A case study 4 • Conclusion 5 9/5/2022 2
  • 3. GPU OVERVIEW 9/5/2022 3 3 Ground power unit (GPU) is a 400 Hz voltage source inverter supplying the airplanes with external electric power during stopovers. Reduce the noise, air pollution. The standard rating of GPU:  115V RMS, 400-Hz with three phase four wires  Power rating: 90 kVA (up to 180 kVA in 1s after starting) Introduction GPU model Control System Design A case study Conclusion
  • 4. 9/5/2022 4 Figure 1: Proposed GPU configuration Improve system reliability in working with unbalanced loads Reduce system volume, size and cost Introduction GPU model Control System Design A case study Conclusion INVERTER TOPOLOGY
  • 5. GPU TRANSFER FUNCTION The PWM function is as follows: 𝐺𝑃𝑊𝑀 = 1 1.5𝑇𝑠𝑠+1 (3) 9/5/2022 5 Introduction GPU model Control System Design A case study Conclusion The state space equation of LC circuit: 𝑑𝑖𝐿 𝑑𝑡 𝑑𝑣𝑂 𝑑𝑡 = −𝑟 𝐿 −1 𝐿 1 𝐶 0 𝑖𝐿 𝑣0 + 1 𝐿 0 0 −1 𝐶 𝑣𝐼 𝑖𝑂 (1) GPU model can be written: 𝑣𝑂 = 𝑣𝐼 𝐿𝐶𝑠2+𝑟𝐶𝑠+1 − (𝑠𝐿+𝑟)𝑖𝑂 𝐿𝐶𝑠2+𝑟𝐶𝑠+1 (2) If consider 𝑖𝑂 are disturbance, the GPU transfer function will be: 𝐺 = 1 𝑁(1.5𝑇𝑠𝑠+1)(𝐿𝐶𝑠2+𝑟𝐶𝑠+1) (4)
  • 6. 9/5/2022 6 OVERALL CONTROL SYSTEM Introduction GPU model Control System Design A case study Conclusion Under the consideration that coupling components is not significantly, can be ignored. Voltage and current loop control have no effect each other, can be designed separately. Figure 2: Overall control system diagram
  • 7. 9/5/2022 7 DEADBEAT CURRENT LOOP CONTROL DESIGN Introduction GPU model Control System Design A case study Conclusion Figure 3: DB current loop Then, the DB controller function is: 𝑅𝑖 𝑧 = 𝑟𝐿 1−𝑒 −𝑟𝐿 𝐿 𝑇𝑠 1−𝑒 −𝑟𝐿 𝐿 𝑇𝑠𝑧−1 1−𝑧−2 (7) The current loop transfer function, can be derived: 𝐻𝑖 𝑧 = 𝑖𝐿 𝑖𝑟𝑒𝑓 = 𝑧−2 (5) The current plant model 𝐺𝑖(𝑧) is determined by [8]: 𝐺𝑖 𝑧 = 1−𝑒 −𝑟𝐿 𝐿 𝑇𝑠 𝑟𝐿 𝑧−1 1−𝑒 −𝑟𝐿 𝐿 𝑇𝑠 𝑧−1 (6)
  • 8. 9/5/2022 8 Figure 4: Discrete parallel resonant voltage controller [2] F. Rojas, R. Cardenas, J. Clare, M. Diaz, J. Pereda and R. Kennel: A Design Methodology of Multiresonant Controllers for High Performance 400 Hz Ground Power Units. IEEE Transactions on Industrial Electronics, vol. 66, no. 8, pp. 6549-6559, Aug. 2019. VOLTAGE RESONANT CONTROL DESIGN The s domain resonant controller transfer function can be written as [3]: 𝑅𝑛(𝑠) = 𝐾𝑟𝑛 𝑠𝑐𝑜𝑠 𝜃𝑛 −𝜔𝑛𝑠𝑖𝑛 𝜃𝑛 𝑠2−𝜔𝑛 2 (8) In which, 𝐾𝑟𝑛 is the gain and 𝜃𝑛 is the resonance frequency for the nth resonant compensator Introduction GPU model Control System Design A case study Conclusion
  • 9. 9/5/2022 9 [3] Z. Li, Y. Li, P. Wang, H. Zhu, C. Liu and F. Gao: Single-Loop Digital Control of High-Power 400-Hz Ground Power Unit for Airplanes. IEEE Transactions on Industrial Electronics, vol. 57, no. 2, pp. 532-543, Feb. 2010. DISCRETE RESONANT CONTROLLER By Zero Order Hold (ZOH) transform, the model of resonant controller in the discrete domain can be obtained [3]: 𝑅𝑧(𝑛) = 𝑧−1 𝑠𝑖𝑛 𝜔𝑛𝑇𝑆 𝑐𝑜𝑠 𝜃𝑛 −(𝑧+1) 1−cos(𝜔𝑛𝑇𝑆) 𝑠𝑖𝑛 𝜃𝑛 𝑧2−2 cos 𝜔𝑛𝑇𝑆 𝑧+1 𝜔𝑛 (9) With 𝑇𝑆 is the system sampling period. Introduction GPU model Resonant controller A case study Conclusion
  • 10. 9/5/2022 10 10 Introduction GPU model Control System Design A case study Conclusion SYSTEM PARAMETERS The system parameters are listed in the Table 1. PARAMETERS VALUE Induction L = 200 µH Capacitance C = 25 µF Inductor resistance 0.02  Switching frequency fc = 18 kHz Output voltage 115V, 400 Hz Transformer ration 5/3 Table 1: System parameters
  • 11. 9/5/2022 11 11 Introduction Inverter topology Control system design A case study Conclusion MATLAB SIMULATION THD = 0.97% Figure 5: Resistive load R = 1.09 with fundamental controller only The case of linear load R = 1.09, only fundamental controller is required.
  • 12. 9/5/2022 12 12 Introduction Inverter topology Control system design A case study Conclusion MATLAB SIMULATION Figure 6: Output voltage with a) only fundamental controller b) with 3rd controller is added THD = 2.26% THD = 1.9% The case of nonlinear load, included a diode rectifier, a capacitor of 50µF and a load 1.09 Ω
  • 13. 9/5/2022 13 13 Introduction Inverter topology Control system design A case study Conclusion MATLAB SIMULATION Figure 7: In the case of a sudden load change a) With DB settling time is 0.035s b) Without DB is 0.08s Figure 5: Output voltage without DB current controller THD = 2.39%
  • 14. 9/5/2022 14 14 Introduction Inverter topology Control system design A case study Conclusion EXPERIMENT SYSTEM DESIGN Figure 8: Experiment system A 90 kVA GPU prototype based on Texas Instrument TMS320F28379D microcontroller was built verify the proposed design method
  • 15. 9/5/2022 15 15 Introduction Inverter topology Control system design A case study Conclusion EXPERIMENT RESULTS Figure 9: Nonlinear load condition with fundamental controller only The case of nonlinear load, only fundamental controller is implemented: THD = 3.29%
  • 16. 9/5/2022 16 16 Introduction Inverter topology Control system design A case study Conclusion EXPERIMENT RESULTS Figure 10: Output voltage under nonlinear load condition with 3rd compensator is added With 3rd compensator is added THD = 2.93% 3rd harmonic = 1.9%
  • 17. 9/5/2022 17 17  A improvement for GPU configuration is proposed enhance the system reliability under unbalanced load conditions, also reduce the volume, size and production cost.  Parallel resonant controller is applied in voltage control loop to control the fundamental voltage also compensate the harmonics.  Deadbeat control algorithm is implemented for inner current loop to remain inductor current stable, contributing to the harmonic distortion compensation at the output voltage  Simulation and experiment results indicate that proposed system can produce a good quality voltage even under the nonlinear load conditions.  Higher order harmonic compensators (5th, 7th) will be next applied to control system to improve the system performance. Introduction Inverter topology Control system design A case study Conclusion CONCLUSION
  • 18. 9/5/2022 18 Thank you for attending! Presenter: Tran Que Son Email: tranqueson.ktdt@tnut.edu.vn