TWM601933U - Motor rotor position detecting device - Google Patents

Abstract

This case proposes a motor rotor position detection device including a magnetic field guiding control circuit and an initial position detection circuit. The magnetic field guiding control circuit receives the test current command and the preset angle, and generates a feedback current according to the test current command and the preset angle. The initial position detection circuit sends a test current command and a preset angle to the magnetic field guide control circuit. The initial position detection circuit includes a current generator, an angle generator and a processing circuit. The current generator outputs the test current command, the angle generator outputs the preset angle, the processing circuit captures the peak value of the feedback current to form a peak value array, and calculates the maximum value of the elements in the peak value array to correspond to one of them The initial angular position of the motor rotor, and before the motor rotates, the initial angular position is sent to the magnetic field guide control circuit.

Description

Motor rotor position detection device

This case is about a motor rotor position detection device, especially a motor rotor initial angular position detection device suitable for a magnetic field-oriented control architecture.

Motors have been widely used in electronic products, such as robotic arms, semiconductor manufacturing and packaging related equipment, elevators, air conditioners, electric vehicles, scanners, printers, optical disc drives, etc. In order to control the normal rotation of the motor, the conventional motor rotor position detection device usually includes a rotor position sensor which is a hardware component to detect the initial position of the motor rotor before the motor rotates, so as to prevent the motor from being started. Unexpected operating conditions.

However, the additional use of the aforementioned rotor position sensor will increase the production cost. If the rotor position sensor is not used, it will cause unexpected operating conditions of the aforementioned motor at startup. Therefore, in order to replace the rotor position sensor, some different motor control technologies have been developed today. However, most of the motor control technologies still require additional hardware circuits, which makes it impossible to effectively reduce the production cost, and the design usually cannot be based on different Motor or different motor application products can be adjusted flexibly.

In one embodiment, a motor rotor position detection device includes a magnetic field guidance control circuit and an initial position detection circuit. The magnetic field guiding control circuit receives the test current command and the preset angle in a preset time interval, and generates a feedback current according to the test current command and the preset angle. The initial position detection circuit sends a test current command and a preset angle to the magnetic field guide control circuit. The initial position detection circuit includes a current generator, an angle generator and a processing circuit. The current generator outputs the test current command, the angle generator outputs the preset angle, the processing circuit captures the peak value of the feedback current to form a peak value array, and calculates a maximum value of the elements in the peak value array. The value corresponds to one of the preset angles to form the initial angular position of the motor rotor, and before the motor rotates, the initial angular position is sent to the magnetic field guide control circuit to control the motor to rotate.

FIG. 1 is a functional block diagram of an embodiment of the motor rotor position detection device 1 and the motor 2 controlled by the motor rotor position detection device 1 according to the present invention. Please refer to FIG. 1, the motor rotor position detecting device 1 includes an initial position detecting circuit 11 and a magnetic field guiding control circuit 12. The motor rotor position detection device 1 can control the rotation of the motor 2 through the driving circuit 3. The motor 2 is suitable for Field Oriented Control (FOC), and the motor rotor position detection device 1 has the aforementioned magnetic field-oriented control function. In an embodiment, the motor 2 may be a brushless DC motor (BLDC) or a permanent-magnet synchronous motor (PMSM). The driving circuit 3 is designed by the manufacturer of the motor 2 and its function is to convert the driving signal transmitted by the motor rotor position detection device 1 into a signal readable by the motor 2 to drive the motor 3 to rotate.

Please continue to refer to Figure 1. The initial position detection circuit 11 is coupled to the magnetic field guiding control circuit 12, and the magnetic field guiding control circuit 12 is coupled to the motor 2. The magnetic field guiding control circuit 12 can determine the torque direction of the rotor (not shown in FIG. 1) of the aforementioned control motor 2 or the direction of the magnetic field generated by the stator (not shown in FIG. 1). Before the rotor of the motor 2 rotates, the initial position detection circuit 11 can generate all test commands within a preset time interval set by the user, which is generally 5-15 milliseconds (ms). The test commands include current commands (with a plurality of direct-axis test current commands S1 and a plurality of quadrature-axis test current commands S3), and a plurality of preset angles θ2. The direct axis test current command S1 is sent from the output terminal P2, the quadrature axis test current command S3 is sent from the output terminal P1, the preset angle θ2 is sent from the output terminal P3, and the three signals (direct axis test current command S1, quadrature axis test The current command S3 and the preset angle θ2) have the same cycle.

Please refer to Figure 3A-3D first. Among them, the initial position detection circuit 11 can generate six direct-axis test current commands S1 and six different preset angles θ2. In addition, the quadrature-axis test current commands S3 are all 0A (amperes) in this embodiment. The initial position detection circuit 11 can send and complete all test commands within 8 milliseconds (a preset time interval). The six direct-axis test current commands S1 respectively occupy six cycle times (cycle 1 to cycle 6), and cycle 1 to cycle 6 can all be 1.3 milliseconds.

In addition, the signals in the same cycle time are named the same ordinal. For example, the direct axis test current command S1 in cycle 1 is named "the first direct axis test current command", and corresponds to the same number in cycle 1. The preset angle θ2 is named "the second preset angle"; and the direct axis test current command S1 and the preset angle θ2 in cycle 2 are named "the second direct axis test current command" and the "second preset angle" respectively. Set the angle", and so on. The so-called correspondence refers to the signals generated in the same cycle, or the signals processed and generated are in the same cycle.

Please refer to FIG. 2, which is a flowchart of an embodiment of the motor rotor position detection method suitable for the motor 2 according to the present application. Please refer to Figure 1 and Figures 3A-3D together. The initial position detection circuit 11 sends a test command (step S01) to the magnetic field guiding control circuit 12 during the preset time interval before the motor 2 rotates. The test command is received within the preset time interval, and the feedback current S2 that can control the rotation of the motor 2 is generated according to the test command (step S02), and the magnetic field guiding control circuit 12 generates the test current command S1 for each axis in the test command Corresponding to a feedback current S2. Therefore, according to the direct-axis test current command S1, the quadrature-axis test current command S3 and the corresponding different preset angles θ2, the magnetic field guiding control circuit 12 generates a plurality of feedback currents S2 with different current peaks. Moreover, because the response time of each feedback current S2 generated by the magnetic field guiding control circuit 12 is 100 microseconds (us), which is a negligible magnitude. In other words, the feedback current S2 and the direct-axis test current command S1 can be almost called "simultaneous generation".

Next, the initial position detection circuit 11 receives a plurality of feedback currents S2 from the magnetic field guiding control circuit 12 (step S03). The initial position detection circuit 11 captures the peak value of each feedback current S2 to form a peak value array, and compares the plurality of returns The peak value between the current S2 is calculated to calculate the maximum element in the peak array (step S04). When the initial position detection circuit 11 calculates the maximum element in the peak array (that is, it is determined that one of the current peaks is the largest), the initial According to the maximum value of the feedback current S2, the position detection circuit 11 corresponds to one of the preset angles θ2 before the motor 2 rotates, and outputs it as the initial angular position θ1 (step S05) to drive The magnetic field guiding control circuit 12 controls the rotation of the motor 2 accordingly. Moreover, because the turnaround time required for the initial position detection circuit 11 to generate the initial angular position θ1 can be in the order of 2 to 8 microseconds, which is a negligible order of magnitude. In other words, the initial position detection circuit 11 can quickly The initial angular position θ1 is calculated.

1 and 3A-3D, the magnetic field guiding control circuit 12 generates six feedback currents S2 with different current peaks according to the six direct-axis test current commands S1 and six preset angles θ2, and the subsequent initial position detection circuit 11 The processing circuit 113 in S2 extracts six feedback currents S2 (units can be amperes) to form a peak array X={3,2,4,6,5,2}, and calculates the maximum element in the peak array X (element) is 6. Next, because the maximum value of 6 is the fourth feedback current, it belongs to cycle 4. Therefore, the processing circuit 113 in the initial position detection circuit 11 will "correspond" to the fourth preset in cycle 4. Angle (that is, 300 degrees), and output the fourth preset angle as the initial angular position θ1, so that the motor 2 runs, and the magnetic field guiding control circuit 12 performs follow-up according to the motor 2 whose rotor initial angular position θ1 is 300 degrees Rotation control.

Therefore, based on the aforementioned FOC control architecture, the initial angular position θ1 of the rotor is detected before the rotor of the motor 2 starts to rotate. In this case, there is no need to add an additional drive current input line to the motor 2 to detect the initial angular position θ1 of the rotor. The current sampling resistor and the corresponding amplifier and digital-to-analog conversion circuit can save additional hardware costs, and the designer can flexibly adjust the number of direct-axis test current commands S1 and quadrature-axis test current commands S3 and each preset angle θ2 In order to improve the accuracy of the motor rotor position detection device 1 to determine the initial angular position θ1 of the rotor, reduce the occurrence of misjudgment of the initial angular position θ1 of the rotor, thereby avoiding unexpected operating conditions of the motor 2 at startup .

In one embodiment, the direct-axis test current command S1 is a current pulse signal, and the initial position detection circuit 11 can determine the current values of the direct-axis test current command S1 and quadrature-axis test current command S3 according to the specifications of the motor 2, and the initial position The detection circuit 11 can receive the input high level time T1 and low level time T2 to adjust the cycle and the duty cycle of the direct-axis test current command S1. For example, taking FIG. 3A as an example, the initial position detection circuit 11 can generate six direct-axis test current commands S1 with current values of 5 amperes, and as shown in FIG. 3A, all six direct-axis test current commands S1 have The high level time T1 and the low level time T2 are the same, so that the six direct-axis test current commands S1 have the same cycle and duty cycle.

Based on the above, please refer to Fig. 2. In step S01, the initial position detection circuit 11 can generate a direct-axis test current command S1 in each cycle, and the initial position detection circuit 11 can generate six direct-axis test currents within six cycles. The test current command S1 and the six preset angles θ2, that is, the aforementioned preset time interval is the sum of the six cycle times, so that the magnetic field guide control circuit 12 will test the current according to the direct-axis test current commands in each of the six cycles. S1 outputs the corresponding feedback current S2. The initial position detection circuit 11 determines the initial angular position θ1 of the rotor after six cycles.

In one embodiment, in order to improve the accuracy of the initial angular position θ1 of the rotor calculated by the initial position detection circuit 11, the angle difference between the two preset angles θ2 sent by the initial position detection circuit 11 in two adjacent periods The value is at least greater than or equal to a preset value set by the user. The preset value can be greater than or equal to 1 degree, and preferably, the preset value is 180 degrees, which can avoid the two preset values in the test command. Assuming that the angle difference of the angle θ2 is too small, resulting in an inaccurate feedback current S2 due to hysteresis, the initial position detection circuit 11 misjudges the current peak value of the feedback current S2 and misjudges the initial angular position θ1 of the rotor.

For details, please refer to Figure 3B. Six preset angles θ2 corresponding to the first preset angle to the sixth preset angle corresponding to the six direct-axis test current commands S1 are 0 degrees, 180 degrees, and 120 degrees. Degrees, 300 degrees, 240 degrees, 60 degrees, it can be seen that the difference between the two preset angles θ2 sent in two adjacent periods is at least greater than or equal to the preset value of 60 degrees. Preferably, the preset value is a combination of angles, namely 180 degrees and 60 degrees, for example, the angle difference between the first preset angle and the second preset angle is 180 degrees, and the second preset angle and the first The angle difference between the three preset angles is 60 degrees, the angle difference between the third preset angle and the fourth preset angle is 180 degrees, and the angle between the fourth preset angle and the fifth preset angle The difference is 60 degrees, and the angle difference between the fifth preset angle and the sixth preset angle is 180 degrees. Accordingly, there can be as large a difference as possible between the two preset angles θ2 generated at different times, so as to prevent the initial position detection circuit 11 from misjudgeting the initial angular position θ1 of the rotor.

As shown in FIG. 1, a driving circuit 3 is still needed to control the rotation of the motor 2, and the driving circuit 3 is coupled to the magnetic field guiding control circuit 12 and the motor 2. The magnetic field guiding control circuit 12 includes a quadrature axis current combining circuit 121, a direct axis current combining circuit 122, a control circuit 123, an Inverse Park Transform calculation circuit 124, a vector generator 125, and a Clarke Transform calculation circuit 126 And Park Transform calculation circuit 127. Among them, the quadrature axis current combining circuit 121, the direct axis current combining circuit 122, the inverse Parker transformation calculation circuit 124 and the Parker transformation calculation circuit 127 are coupled to the initial position detection circuit 11. The control circuit 123, the inverse Parker conversion calculation circuit 124, and the vector generator 125 are sequentially coupled between the quadrature axis current combining circuit 121 and the driving circuit 3, and the control circuit 123, the inverse Parker conversion calculation circuit 124, and the vector generator 125 are coupled It is connected between the direct-axis current combining circuit 122 and the driving circuit 3. The Clark conversion calculation circuit 126 is coupled to the driving circuit 3 and the motor 2. The Parker conversion calculation circuit 127 is coupled between the Clark conversion calculation circuit 126 and the quadrature axis current combining circuit 121, and is coupled between the Clark conversion calculation circuit 126 and the direct axis current combining circuit 122. The initial position detection circuit 11 includes output terminals P1, P2, P3, and P4. The output terminal P1 is coupled to the quadrature axis current combining circuit 121, the output terminal P2 is coupled to the direct axis current combining circuit 122, and the output terminal P3 is coupled to the Parker conversion calculation circuit 127. And the reverse Parker conversion calculation circuit 124.

Please refer to Figure 1 to Figure 4 in the follow-up. Wherein, in one embodiment, in step S01, the current value of the quadrature axis test current command S3 output by the output terminal P1 of the initial position detection circuit 11 is 0 ampere, and is output by the output terminal P2 of the initial position detection circuit 11 The direct-axis test current command S1 is sent to the magnetic field guiding control circuit 12, and the output terminal P3 of the initial position detection circuit 11 outputs a plurality of preset angles θ2 to the inverse Parker conversion calculation circuit 124 and the Parker conversion calculation circuit 127. Next, in step S02, the quadrature axis current combining circuit 121 of the magnetic field guiding control circuit 12 receives the quadrature axis test current command S3 from the output terminal P1 of the initial position detection circuit 11, and receives the quadrature axis feedback current from the Parker conversion calculation circuit 127 S4 (Before the rotor of the motor 2 rotates, the current value of the quadrature axis feedback current S4 can have an initial value, and the aforementioned initial value can be zero) (step S021), the quadrature axis current combining circuit 121 will test the quadrature axis current Command S3 and quadrature axis feedback current S4 are combined and output. And, taking FIGS. 3A-3D as an example, the direct-axis current combining circuit 122 receives six direct-axis test current commands S1 from the output terminal P2 of the initial position detection circuit 11 during the six cycles specified by the developer, and converts them from Parker. The calculation circuit 127 receives the feedback current S2 as the direct-axis feedback current (before the rotor of the motor 2 rotates, the current value of the feedback current S2 may have an initial value, and the aforementioned initial value may be zero) (step S021) , The direct-axis current combining circuit 122 combines the direct-axis test current command S1 and the feedback current S2 to output.

……(1.1) In each of the six cycles, the control circuit 123 generates a direct-axis voltage signal Vd and a quadrature-axis voltage signal Vq corresponding to the direct current signal based on the output signal of the quadrature-axis current combining circuit 121 and the output signal of the direct-axis current combining circuit 122 (Step S022). The reverse Parker conversion calculation circuit 124 then uses the direct-axis voltage signal Vd, the quadrature-axis voltage signal Vq, and the six preset angles θ2 sent by the initial position detection circuit 11 in six cycles in each of the six cycles, based on Equation 1.1 Perform reverse Parker transformation (step S023) to calculate the two AC voltage signals Vα and Vβ corresponding to the two-phase stationary coordinate axis in each cycle. Then, the vector generator 125 performs space vector pulse width modulation on the AC voltage signals Vα and Vβ in each of the six cycles to control the required duty cycle of the three phases and output switching signals Ta, Tb, Tc To the drive circuit 3 including the inverter (step S024), the drive circuit 3 generates three-phase AC currents Ia, Ib and Ic are the motor drive currents (step S025) to drive the rotor of the motor 2 to rotate.

……(1.1)

……(1.2)

……(1.3) While the rotor of the motor 2 is rotating, the magnetic field guiding control circuit 12 will capture the three-phase AC currents Ia, Ib, Ic, and through the Clark conversion calculation circuit 126 in each of the six cycles to execute Clark based on formula 1.2 Conversion (step S026) to convert the three-phase AC currents Ia, Ib, and Ic into two AC currents Iα, Iβ corresponding to the two-phase stationary coordinate axis. The Parker conversion calculation circuit 127 performs Parker conversion in each of the six cycles (step S027) to convert the AC currents Iα, Iβ and the preset angle θ2 into corresponding synchronous rotation coordinate axes based on formula 1.3 It is the quadrature axis feedback current S4 and the feedback current S2 of the direct current. In step S03, the initial position detection circuit 11 receives the six feedback currents S2 corresponding to the d-axis of the synchronous rotation coordinate axis from the Parker conversion calculation circuit 127, To determine which of the six feedback currents S2 generated by the Parker conversion calculation circuit 127 within the preset time interval has the largest current peak value, the output terminal P4 outputs the initial angular position θ1 of the rotor.

……(1.2)

……(1.3)

Finally, after the initial position detection circuit 11 calculates the initial angular position θ1, it can be transmitted to other components, and other components can send the initial angular position θ1 and the direct axis input current command and quadrature axis input current command required during operation to The magnetic field guiding control circuit 12 enables the magnetic field guiding control circuit 12 to control the rotation of the motor 2 accordingly, thereby avoiding unexpected operating conditions when the motor 2 starts to rotate.

The number of direct-axis test current commands S1 has a great relationship with accuracy. As shown in Figure 3A, when the number of direct-axis test current commands S1 is set to six, it means that a circle (rotor track) is divided into six positioning points, and the accuracy of the positioning points is 60 degrees. In other embodiments, the number of the direct-axis test current commands S1 ranges from two to three hundred and sixty, preferably two to twelve, and most preferably six. For example, when the number of direct-axis test current commands S1 is set to ten, it means that a circle (rotor track) is divided into ten positioning points. The positioning point accuracy is 36 degrees, which is more accurate. The designer of the motor rotor position detection device 1 can design the number of the direct-axis test current command S1 and the corresponding preset angle θ2 according to the desired accuracy of the initial angular position θ1.

In one embodiment, the circuit structure of the inverter included in the driving circuit 3 can be referred to FIG. 5. As can be seen from FIG. 5, there is no need to set any resistors in the driving circuit 3 to sample the three-phase AC currents Ia, Ib, Ic. , And there is no need to additionally provide amplifiers or digital-to-analog converters (DACs) connected to the sampling current resistors for sampling the three-phase alternating currents Ia, Ib, and Ic, thus further saving additional hardware costs and circuit space.

In one embodiment, please refer to FIGS. 1 and 6 together. The initial position detection circuit 11 further includes a current generator 111, an angle generator 112, and a processing circuit 113. The processing circuit 113 is coupled to the current generator 111 and the angle generator 112. . The processing circuit 113 can control the current generator 111 to output a plurality of direct-axis test current commands S1 in each cycle within the preset time interval based on the high level time T1 and the low level time T2, and the processing circuit 113 can control the angle generator 112 to preset Each cycle output in the time interval corresponds to the preset angle θ2 of each linear axis test current command S1. In addition, the processing circuit 113 may receive the feedback current S2 from the Parker conversion calculation circuit 127, and determine the current peak value of the feedback current S2 received in each cycle to determine which current of the feedback current S2 in the preset time interval The peak value is the maximum, and the corresponding initial angular position θ1 is output. The processing circuit 113 can control the current generator 111, the angle generator 112 and perform the output of the initial angular position θ1 based on a finite state machine (FSM). In one embodiment, the control circuit 123 may be a closed loop controller suitable for direct-axis current and quadrature-axis current, such as a PID controller.

In addition, the value range of the initial angular position θ1 and the preset angle θ2 are all virtual vectors for calculations defined by the initial position circuit 11, the inverse Parker conversion calculation circuit 124, and the Parker conversion calculation circuit 127. Space (virtual vector space) (this vector space system is called domain). Therefore, in the embodiment, the initial angular position θ1 output by the initial position detection circuit 11 can be output to the inverse Parker conversion calculation circuit 124 for calculation during the actual operation of the motor 2. In another embodiment, the user can connect an external conversion circuit (not shown in Figure 1) to the output P4 to convert the virtual vector space into a real space, so that the initial angular position θ1 can be converted into a real space After the three-dimensional coordinates in, follow-up processing.

In addition, the initial position detection circuit 11 and the magnetic field guidance control circuit 12 can be implemented by a microcontroller (MCU) or other controllers with control and data computing capabilities. The designer can use the architecture disclosed in Figure 1, Figure 5 and Figure 6 to make a chip, or use the control method disclosed in Figure 2 to Figure 4 to write the program code and burn it into the platform provided by the manufacturer to form Application on the platform, this application can obtain the initial position of the motor (rotor) in real time. Because generally the existing platform can only be used to control the motor speed, if the initial position of the motor is required, additional hardware circuits must be installed. If you want to know the initial position when using a general existing platform and do not want to install additional devices, you only need to use or use the application program formed by the control method disclosed in Figures 2 to 4 combined with the motor rotor position detection device 1. You can know the initial position of the motor rotor, which is very convenient.

To sum up, according to an embodiment of the motor rotor position detection device of the present invention, the initial position detection circuit can replace the general commercially available rotor position sensor, and the initial position detection circuit can be well combined with the magnetic field guidance control circuit. The initial angular position of the motor rotor is detected. The designer of the motor rotor position detection device does not need to adjust the magnetic field guidance control circuit. When the motor rotor position detection device is implemented by a microcontroller, the designer does not need to modify the magnetic field guidance control. The code of the magnetic field-oriented control executed by the circuit.

In addition, the designer can flexibly adjust the number of test current commands and the angle value of each preset angle to reduce the misjudgment of the initial angular position of the rotor, and there is no need to add additional current sampling resistors on the motor bus current input line And the corresponding amplifier and digital-to-analog conversion circuit can further save additional hardware costs.

Although this case has been disclosed by the examples above, it is not intended to limit the case. Anyone with ordinary knowledge in the technical field can make some changes and modifications without departing from the spirit and scope of the case. Therefore, the scope of protection of this case The scope of the patent application attached hereafter shall prevail.

1: Motor rotor position detection device 11: Initial position detection circuit 111: current generator 112: Angle generator 113: Processing circuit 12: Magnetic field guide control circuit 121: Quadrature axis current combining circuit 122: Direct axis current combining circuit 123: control circuit 124: Reverse Parker conversion calculation circuit 125: Vector generator 126: Clark conversion calculation circuit 127: Parker conversion calculation circuit 2: motor 3: drive circuit S1: Direct axis test current command S2: Feedback current S3: Quadrature axis test current command S4: Quadrature axis feedback current Vd: Direct axis voltage signal Vq: Quadrature axis voltage signal Vα: AC voltage signal Vβ: AC voltage signal Ia: Three-phase AC current Ib: Three-phase AC current Ic: Three-phase AC current Iα: AC current Iβ: AC current T1: High level time T2: Low level time Ta: switch signal Tb: switch signal Tc: switch signal θ1: Initial angular position θ2: preset angle P1~P4: output terminal S01~S05: Step S021~S027: steps

[Figure 1] is a functional block diagram of an embodiment of the motor rotor position detection device and the motor controlled by the motor rotor position detection device according to the present invention. [Figure 2] is a flow chart of an embodiment of a motor rotor position detection method suitable for a motor according to the present application. [FIGS. 3A-3D] are waveform diagrams of one embodiment of test current command, preset angle, feedback current and initial angular position in FIG. 1. [Figure 4] is a flowchart of an embodiment of one of the steps in Figure 2. [Fig. 5] is a circuit diagram of an embodiment of the driving circuit in Fig. 1. [Fig. [Fig. 6] is a functional block diagram of an embodiment of the initial position detection circuit in Fig. 1.

1: Motor rotor position detection device

11: Initial position detection circuit

12: Magnetic field guide control circuit

121: Quadrature axis current combining circuit

122: Direct axis current combining circuit

123: control circuit

124: Reverse Parker conversion calculation circuit

125: Vector generator

126: Clark conversion calculation circuit

127: Parker conversion calculation circuit

2: motor

3: drive circuit

S1: Direct axis test current command

S2: Feedback current

S3: Quadrature axis test current command

S4: Quadrature axis feedback current

Vd: Direct axis voltage signal

Vq: Quadrature axis voltage signal

Vα: AC voltage signal

Vβ: AC voltage signal

Ia: Three-phase AC current

Ib: Three-phase AC current

Ic: Three-phase AC current

Iα: AC current

Iβ: AC current

T1: High level time

T2: Low level time

Ta: switch signal

Tb: switch signal

Tc: switch signal

θ1: Initial angular position

θ2: preset angle

P1~P4: output terminal

Claims (9)

A motor rotor position detection device, including: A magnetic field-oriented control circuit is used to receive a test command within a preset time interval and generate a feedback current according to the test command, wherein the test command includes a test current command and a preset angle; and An initial position detection circuit is used to send the test command to the magnetic field guidance control circuit and an initial angular position of the motor rotor. The initial position detection circuit is coupled to the magnetic field guidance control circuit and includes: A current generator for outputting the test current command; An angle generator for outputting the preset angle; and A processing circuit, coupled to the current generator and the angle generator, is used to capture the peak value of the feedback current to form a peak value array, and calculate a maximum value of the elements in the peak value array, and according to the maximum value The value corresponds to one of the preset angles to form the initial angular position, and before a motor rotates, the initial angular position is sent to the magnetic field guiding control circuit to control the motor to rotate. The motor rotor position detection device according to claim 1, wherein the initial position detection circuit sends the test command in a plurality of cycles, and the difference between the two preset angles issued in two adjacent cycles The difference is greater than or equal to a preset value. The motor rotor position detection device according to claim 2, wherein the preset value is greater than or equal to 1 degree. The motor rotor position detection device according to claim 1, wherein the magnetic field guiding control circuit includes: A straight-axis current combining circuit coupled to the initial position detection circuit, the straight-axis current combining circuit for receiving the test current command; and A quadrature axis current combining circuit coupled to the initial position detection circuit; The test current command includes a current pulse signal of a high level time and a low level time. The motor rotor position detecting device according to claim 4, wherein the processing circuit further receives the high level time and the low level time to control the current generator to generate the corresponding test current command. The motor rotor position detection device according to claim 4, wherein the magnetic field guiding control circuit further includes a Parker conversion calculation circuit coupled to the direct-axis current combining circuit, the quadrature-axis current combining circuit and the initial position detection circuit , The Parker conversion calculation circuit is used to transmit the feedback current to the direct-axis current combining circuit and the initial position detection circuit. According to the motor rotor position detection device of claim 4, the magnetic field guiding control circuit further includes: A Parker conversion calculation circuit coupled to the initial position detection circuit, the direct-axis current combining circuit and the quadrature-axis current combining circuit; and An inverse Parker conversion calculation circuit, coupled to the initial position detection circuit, the direct-axis current combining circuit, and the quadrature-axis current combining circuit; Wherein, the angle generator outputs the predetermined angle to the Parker conversion calculation circuit and the reverse Parker conversion calculation circuit, so that the Parker conversion calculation circuit generates the feedback current accordingly. The motor rotor position detection device according to claim 1, wherein the magnetic field-oriented control circuit includes an inverse Parker conversion calculation circuit, and the processing circuit sends the initial angular position to the inverse Parker conversion calculation circuit to calculate the motor The rotation control. The motor rotor position detection device according to claim 1, wherein the magnetic field guiding control circuit includes: A straight axis current combining circuit, coupled to the initial position detection circuit, and receiving the test current command; A quadrature axis current combining circuit, coupled to the initial position detection circuit, and receiving a zero current value; An inverse Parker conversion calculation circuit, coupled to the initial position detection circuit, the direct-axis current combining circuit, and the quadrature-axis current combining circuit, to receive the predetermined angle from the angle generator; and A Parker conversion calculation circuit, coupled to the initial position detection circuit, the direct-axis current combining circuit, and the quadrature-axis current combining circuit, receives the predetermined angle from the angle generator to generate the feedback current, and transmits the feedback Current is supplied to the direct-axis current combining circuit and the processing circuit.

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