JAJU802A January   2022  – October 2022

 

  1.   概要
  2.   リソース
  3.   特長
  4.   アプリケーション
  5.   5
  6. 1System Description
    1. 1.1 Key System Specifications
  7. 2System Overview
    1. 2.1 Block Diagram
    2. 2.2 Design Considerations
    3. 2.3 Highlighted Products
      1. 2.3.1 TMS320F2800137
      2. 2.3.2 TMS320F280025C
      3. 2.3.3 TMS320F280039C
      4. 2.3.4 UCC28740
      5. 2.3.5 UCC27517
      6. 2.3.6 TLV9062
      7. 2.3.7 TLV76733
    4. 2.4 System Design Theory
      1. 2.4.1 Interleaved PFC
        1. 2.4.1.1 Full Bridge Diode Rectifier Rating
        2. 2.4.1.2 Inductor Ratings
        3. 2.4.1.3 AC Voltage Sensing
        4. 2.4.1.4 DC Link Voltage Sensing
        5. 2.4.1.5 Bus Current Sensing
        6. 2.4.1.6 DC Link Capacitor Rating
        7. 2.4.1.7 MOSFET Ratings
        8. 2.4.1.8 Diode Ratings
      2. 2.4.2 Three-Phase PMSM Drive
        1. 2.4.2.1 Field Oriented Control of PM Synchronous Motor
        2. 2.4.2.2 Sensorless Control of PM Synchronous Motor
          1. 2.4.2.2.1 Enhanced Sliding Mode Observer with Phase Locked Loop
            1. 2.4.2.2.1.1 Mathematical Model and FOC Structure of an IPMSM
            2. 2.4.2.2.1.2 Design of ESMO for the IPMSM
            3. 2.4.2.2.1.3 Rotor Position and Speed Estimation with PLL
        3. 2.4.2.3 Field Weakening (FW) and Maximum Torque Per Ampere (MTPA) Control
        4. 2.4.2.4 Compressor Drive with Automatic Vibration Compensation
        5. 2.4.2.5 Fan Drive with Flying Start
        6. 2.4.2.6 Hardware Prerequisites for Motor Drive
          1. 2.4.2.6.1 Motor Current Feedback
            1. 2.4.2.6.1.1 Current Sensing with Three-Shunt
            2. 2.4.2.6.1.2 Current Sensing with Single-Shunt
          2. 2.4.2.6.2 Motor Voltage Feedback
  8. 3Hardware, Software, Testing Requirements, and Test Results
    1. 3.1 Getting Started Hardware
      1. 3.1.1 Hardware Board Overview
      2. 3.1.2 Test Conditions
      3. 3.1.3 Test Equipment Required for Board Validation
      4. 3.1.4 Test Setup
    2. 3.2 Getting Started Firmware
      1. 3.2.1 Download and Install Software Required for Board Test
      2. 3.2.2 Opening Project Inside CCS
      3. 3.2.3 Project Structure
    3. 3.3 Test Procedure
      1. 3.3.1 Build Level 1: CPU and Board Setup
        1. 3.3.1.1 Start CCS and Open Project
        2. 3.3.1.2 Build and Load Project
        3. 3.3.1.3 Setup Debug Environment Windows
        4. 3.3.1.4 Run the Code
      2. 3.3.2 Build Level 2: Open Loop Check with ADC Feedback
        1. 3.3.2.1 Start CCS and Open Project
        2. 3.3.2.2 Build and Load Project
        3. 3.3.2.3 Setup Debug Environment Windows
        4. 3.3.2.4 Run the Code
      3. 3.3.3 Build Level 3: Closed Current Loop Check
        1. 3.3.3.1 Start CCS and Open Project
        2. 3.3.3.2 Build and Load Project
        3. 3.3.3.3 Setup Debug Environment Windows
        4. 3.3.3.4 Run the Code
      4. 3.3.4 Build Level 4: Full PFC and Motor Drive Control
        1. 3.3.4.1  Start CCS and Open Project
        2. 3.3.4.2  Build and Load Project
        3. 3.3.4.3  Setup Debug Environment Windows
        4. 3.3.4.4  Run the Code
        5. 3.3.4.5  Run the System
        6. 3.3.4.6  Tuning Motor Drive FOC Parameters
        7. 3.3.4.7  Tuning PFC Parameters
        8. 3.3.4.8  Tuning Field Weakening and MTPA Control Parameters
        9. 3.3.4.9  Tuning Flying Start Control Parameters
        10. 3.3.4.10 Tuning Vibration Compensation Parameters
        11. 3.3.4.11 Tuning Current Sensing Parameters
    4. 3.4 Test Results
      1. 3.4.1 Performance Data and Curves
      2. 3.4.2 Functional Waveforms
      3. 3.4.3 Transient Waveforms
      4. 3.4.4 MCU CPU Load, Memory and Peripherals Usage
        1. 3.4.4.1 CPU Load for Full Implementation
        2. 3.4.4.2 Memory Usage
        3. 3.4.4.3 Peripherals Usage
    5. 3.5 Migrate Firmware to a New Hardware Board
      1. 3.5.1 Configure the PWM, CMPSS, and ADC Modules
      2. 3.5.2 Setup Hardware Board Parameters
      3. 3.5.3 Configure Faults Protection Parameters
      4. 3.5.4 Setup Motor Electrical Parameters
      5. 3.5.5 Setup PFC Control Parameters
  9. 4Design and Documentation Support
    1. 4.1 Design Files
      1. 4.1.1 Schematics
      2. 4.1.2 Bill of Materials
      3. 4.1.3 Altium Project
      4. 4.1.4 Gerber Files
      5. 4.1.5 PCB Layout Guidelines
    2. 4.2 Software Files
    3. 4.3 Documentation Support
    4. 4.4 サポート・リソース
    5. 4.5 Trademarks
  10. 5Terminology
  11. 6Revision History

Field Weakening (FW) and Maximum Torque Per Ampere (MTPA) Control

Permanent magnet synchronous motor (PMSM) is widely used in home appliance applications due to its high power density, high efficiency, and wide speed range. The PMSM includes two major types: the surface-mounted PMSM (SPM), and the interior PMSM (IPM). SPM motors are easier to control due to their linear relationship between the torque and q-axis current. However, the IPMSM has electromagnetic and reluctance torques due to a large saliency ratio. The total torque is non-linear with respect to the rotor angle. As a result, the MTPA technique can be used for IPM motors to optimize torque generation in the constant torque region. The aim of the field weakening control is to optimize to reach the highest power and efficiency of a PMSM drive. Field weakening control can enable a motor operation over its base speed, expanding its operating limits to reach speeds higher than rated speed and allow optimal control across the entire speed and voltage range.

The voltage equations of the mathematical model of an IPMSM can be described in d-q coordinates as shown in Equation 66 and Equation 67.

Equation 66. vd=Lddiddt+Rsid-pωmLqiq 
Equation 67. vq=Lqdiqdt+Rsiq+pωmLdid+pωmψm

The dynamic equivalent circuit of an IPM synchronous motor is shown in Figure 2-22.

Figure 2-22 Equivalent Circuit of an IPM Synchronous Motor

The total electromagnetic torque generated by the IPMSM can be expressed as Equation 68 that the produced torque is composed of two distinct terms. The first term corresponds to the mutual reaction torque occurring between torque current iq and the permanent magnet ψm, while the second term corresponds to the reluctance torque due to the differences in d-axis and q-axis inductance.

Equation 68. Te=32p ψmiq+(Ld-Lq)idiq

In most applications, IPMSM drives have speed and torque constraints, mainly due to inverter or motor rating currents and available DC link voltage limitations respectively. These constraints can be expressed with the mathematical equations Equation 69 and Equation 70.

Equation 69. Ia=id2+iq2Imax
Equation 70. Va=vd2+vq2Vmax

Where Vmaxand Imax are the maximum allowable voltage and current of the inverter or motor. In a two-level three-phase Voltage Source Inverter (VSI) fed machine, the maximum achievable phase voltage is limited by the DC link voltage and the PWM strategy. The maximum voltage is limited to the value as shown in Equation 71 if Space Vector Modulation (SVPWM) is adopted.

Equation 71. vd2+vq2vmax=vdc3

Usually the stator resistance Rs is negligible at high speed operation and the derivate of the currents is zero in steady state, thus Equation 72 is obtained as shown.

Equation 72. Ld2(id+ψpmLd)2+Lq2iq2 Vmaxωm

The current limitation of Equation 69 produces a circle of radius Imax in the d-q plane, and the voltage limitation of Equation 71 produces an ellipse whose radius Vmax decreases as speed increases. The resultant d-q plane current vector must be controlled to obey the current and voltage constraints simultaneously. According to these constraints, three operation regions for the IPMSM can be distinguished as shown in Figure 2-23.

Figure 2-23 IPMSM Control Operation Regions
  1. Constant Torque Region: MTPA can be implemented in this operation region to ensure maximum torque generation.
  2. Constant Power Region: Field weakening control must be employed and the torque capacity is reduced as the current constraint is reached.
  3. Constant Voltage Region: In this operation region, deep field weakening control keeps a constant stator voltage to maximize the torque generation.

In the constant torque region, according to Equation 68, the total torque of an IPMSM includes the electromagnetic torque from the magnet flux linkage and the reluctance torque from the saliency between Ld and Lq. The electromagnetic torque is proportional to the q-axis current iq, and the reluctance torque is proportional to the multiplication of the d-axis current id, the q-axis current iq, and the difference between Ld and Lq.

Conventional vector control systems of a SPM motors only utilizes electromagnetic torque by setting the commanded id to zero for non-field weakening modes. But an IPMSM will utilize the reluctance torque of the motor, d-axis current should be controlled as well. The aim of the MTPA control is to calculate the reference currents id and iq to maximize the ratio between produced electromagnetic torque and reluctance torque. The relationship between id and iq, and the vectorial sum of the stator current Is is shown in the following equations.

Equation 73. Is=id2+iq2
Equation 74. Id=Iscosβ
Equation 75. Iq=Issinβ

Where β is the stator current angle in the synchronous (d-q) reference frame. Equation 68 can be expressed as Equation 76 where Is substituted for id and iq.

Equation 76 shows that motor torque depends on the angle of the stator current vector; as such

Equation 76. Te=32pIssinβ ψm+(Ld-Lq)Iscosβ

, the maximum efficiency point can be calculated when the motor torque differential is equal to zero. The MTPA point can be found when this differential, dTedβis zero as given in Equation 77.

Equation 77. dTedβ=32p ψmIscosβ+(Ld-Lq)Is2cos2β=0 

Following, the current angle of the MTPA control can be derived as in Equation 78.

Equation 78. βmtpa=cos-1-ψm+ψm2+8*Ld-Lq2*Is24*Ld-Lq*Is

Thus, the effective d-axis and q-axis reference currents can be expressed by Equation 79 and Equation 80 using the current angle of the MTPA control.

Equation 79. Id=Is*cosβmtpa
Equation 80. Iq=Is*sinβmtpa

However, as shown in Equation 78, the angle of the MTPA control, βmtpa is related to d-axis and q-axis inductance. This means that the variation of inductance will impede the ability to find the optimal MTPA point. To improve the efficiency of a motor drive, the d-axis and q-axis inductance should be estimated online, but the parameters Ld and Lq are not easily measured online and are influenced by saturation effects. A robust Look-Up Table (LUT) method ensures controllability under electrical parameter variations. Usually, to simplify the mathematical model, the coupling effect between d-axis and q-axis inductance can be neglected. Thus, assumes that Ld changes with id only, and Lq changes with iq only. Consequently, d- and q-axis inductance can be modeled as a function of their d-q currents respectively, as shown in Equation 81 and Equation 82.

Equation 81. Ld=f1id, iq=f1id
Equation 82. Lq=f2iq, id=f2iq

To reduce the ISR calculation burden by simplifying Equation 78. The motor-parameter-based constant, Kmtpa is expressed instead as Equation 84, where Kmtpa is computed in the background loop using the updated Ld and Lq.

Equation 83. Kmtpa=ψm4*Lq-Ld=0.25*ψmLq-Ld
Equation 84. βmtpa=cos-1Kmtpa/Is-Kmtpa/Is2+0.5

A second intermediate variable, Gmtpa described in Equation 85, is defined to further simplify the calculation. Using Gmtpa, the angle of the MTPA control, βmtpa can be calculated as Equation 86. These two calculations are performed in the ISR to achieve a real current angle βmtpa.

Equation 85. Gmtpa=Kmtpa/Is
Equation 86. βmtpa=cos-1Gmtpa-Gmtpa2+0.5

In all cases, the magnetic flux can be weakened to extend the achievable speed range by acting on the direct axis current id. As a consequence of entering this constant power operating region, field weakening control is chosen instead of the MTPA control used in constant power and voltage regions. Since the maximum inverter voltage is limited, PMSM motors cannot operate in such speed regions where the back-electromotive force, almost proportional to the permanent magnet field and motor speed, is higher than the maximum output voltage of the inverter. The direct control of magnet flux is not an option in PM motors. However, the air gap flux can be weakened by the demagnetizing effect due to the d-axis armature reaction by adding a negative id. Considering the voltage and current constraints, the armature current and the terminal voltage are limited as Equation 69 and Equation 70. The inverter input voltage (DC-Link voltage) variation limits the maximum output of the motor. Furthermore, the maximum fundamental motor voltage also depends on the PWM method used. In Equation 72, the IPMSM has two factors: one is a permanent magnet value and the other is made by inductance and current of flux.

Figure 2-24 shows the typical control structure is used to implement field weakening. βfw is the output of the field weakening (FW) PI controller and generates the reference id and iq. Before the voltage magnitude reaches its limit, the input of the PI controller of FW is always positive and therefore the output is always saturated at 0.

Figure 2-24 Block Diagram of Field-Weakening and Maximum Torque per Ampere Control

Figure 2-13 and Figure 2-15 show the implementation of FAST or eSMO based FOC block diagram. The block diagrams provide an overview of the FOC system's functions and variables. There are two control modules in the motor drive FOC system: one is MTPA control and the other one is field weakening control. These two modules generate current angle βmtpa and βfw respectively based on input parameters as show in Figure 2-25.

Figure 2-25 Current Phasor Diagram of an IPMSM During FW and MTPA

The switching control module is used to decide which angle should be applied, and then calculate the reference idand iq as shown in Equation 74 and Equation 75. The current angle is chosen as following Equation 87 and Equation 88.

Equation 87. β=βfw if βfw>βmtpa
Equation 88. β=βmpta if βfw<βmtpa

Figure 2-26 is the flowchart that shows the steps required to run InstaSPIN-FOC with FW and MPTA in the main loop and interrupt.

Figure 2-26 Flowchart for an InstaSPIN-FOC Project with FW and MTPA