This application is a National Stage of International Application No. PCT/JP2018/046482 filed Dec. 18, 2018.
The present application relates to an angle detection device, and to an electric power steering device in which the angle detection device is used.
In general, a resolver or an MR (magnetoresistance) sensor is widely used as an angle detector that detects an angle of rotation of a rotating machine, for example, a motor. These angle detectors are such that a sine signal and a cosine signal in accordance with a motor angle of rotation are output, but when an error (an offset component or a harmonic component) is included in the sine signal or the cosine signal, or when amplitude values of the sine signal and the cosine signal differ, a detected angle value obtained from the sine signal and the cosine signal has an error with respect to an actual motor angle of rotation, because of which a problem occurs in that a motor control performance is caused to worsen.
In response to this, Patent Literature 1 discloses an angle detection device wherein a center point correction value of a sine signal and a cosine signal of a resolver is stored in advance in an EEPROM (electrically erasable programmable read-only memory) or the like, or a peak value and a trough value of a sine signal and a cosine signal are read, a center point correction value is obtained from a difference between a center point of the peak value and the trough value and a preset predetermined center point value, a correction is implemented by adding the center point correction value to the sine signal and the cosine signal, and a motor angle signal is calculated from the corrected sine signal and cosine signal.
Also, Patent Literature 2 discloses an angle detection device wherein an offset correction value with respect to a sine signal and a cosine signal is obtained using an angle error wherein a frequency component lower than an electrical angle frequency component of an angle signal is removed from the angle signal, and a component equal to or higher than the frequency of the electrical angle frequency component is extracted, whereby, even when a secondary component occurs in addition to a center point error in the sine signal and the cosine signal, an electrical angle frequency component of the angle signal caused by the secondary component and the center point error can be corrected.
The angle detection device disclosed in Patent Literature 1 is such that when a harmonic component exists in the sine signal and the cosine signal, or when orthogonality is low, there is a problem in that an angle error (which is a discrepancy between a detected angle value and a motor angle of rotation) occurring as a result thereof cannot be corrected. Herein, orthogonality indicates an index of deviation of a phase difference between the sine signal and the cosine signal from 90 degrees, which is ideal, and means that the phase difference between the sine signal and the cosine signal is in a vicinity of 90 degrees when orthogonality is high, and the phase difference between the sine signal and the cosine signal is deviating from 90 degrees when orthogonality is low.
Also, the angle detection device disclosed in Patent Literature 2 is such that although an electrical angle frequency component of an angle signal can be corrected well, there is no advantage with respect to a component of another order.
The present application discloses technology for resolving the aforementioned kinds of problem, and has an object of providing an angle detection device such that an angle error is restricted even when a harmonic component exists in a sine signal or a cosine signal or when orthogonality is low, and with respect to an angle signal component of an order other than that of an electrical angle frequency component, and of providing an electric power steering device in which the angle detection device is used.
An angle detection device disclosed in the present application is an angle detection device that outputs a detected angle value from an angle signal of a rotating body, and includes an angle corrector that carries out each of an operation obtaining a first n-fold angle signal by multiplying the angle signal by n (n is a real number other than 1), an operation obtaining, based on the first n-fold angle signal, a first sine wave signal and a second sine wave signal of mutually differing phases, an operation obtaining a second n-fold angle signal based on the first sine wave signal and the second sine wave signal, an operation obtaining a first offset correction value, which is an offset correction value of the first sine wave signal, based on the second n-fold angle signal and obtaining a second offset correction value, which is an offset correction value of the second sine wave signal, based on the second n-fold angle signal, and an operation correcting the second n-fold angle signal based on the first sine wave signal corrected by the first offset correction value and the second sine wave signal corrected by the second offset correction value, wherein the angle correction device outputs the detected angle value based on the corrected second n-fold angle signal.
According to the angle detection device disclosed in the present application, an angle detection device such that an angle error is restricted even when a harmonic component exists in a sine signal and a cosine signal or when orthogonality is low, and with respect to an angle signal component of an order other than that of an electrical angle frequency component, can be provided.
The foregoing and other objects, features, aspects, and advantages of the present application will become more apparent from the following detailed description of the present application when taken in conjunction with the accompanying drawings.
Hereafter, preferred embodiments of an angle detection device according to the present application, and of an electric power steering device in which the angle detection device is used, will be described using the drawings. In the drawings, identical reference signs indicate identical or corresponding portions.
By the excitation coil 5 being driven using an alternating current signal shown in
The angle detecting means 4a includes an A/D converter 8 that has an output of the differential amplifier 3 as an input, an angle calculator 9 that has the sine signal S(θ) and the cosine signal C(θ), which are outputs of the A/D converter 8, as inputs, and an angle corrector 10 that has an angle signal θr output from the angle calculator 9 as an input.
The angle detection device 100A is configured as heretofore described, and next, a method of processing a signal output from the resolver 1 will be described.
The excitation coil 5 of the resolver 1 is driven by the excitation circuit 2 using the alternating current signal shown in
The angle calculating means 4a carries out an A/D conversion of peak points of sine values and cosine values indicated by circles in
Next, an operation carried out in the angle corrector 10 will be described, based on
The angle corrector 10 is configured to include a first multiplier 101, a sine unit 102, a cosine unit 103, an adder 104, a tripled angle calculator 105, an offset correction value calculator 106, a second multiplier 107, and an offset angle calculator 108.
The angle corrector 10 is configured of a processor P and a storage device M, as in a hardware example shown in
The first multiplier 101 triples and outputs the angle signal θr output from the angle calculator 9. This output value is defined as a first tripled angle signal 3θr. As the first tripled angle signal 3θr is simply such that the angle signal θr is tripled, it is depicted as in b of
Next, the sine unit 102 outputs a sine value with respect to the first tripled angle signal 3θr. The output of the sine unit 102 is a first sine wave signal S(3θr). The cosine unit 103 outputs a cosine value with respect to the first tripled angle signal 3θr. The output of the cosine unit 103 is a second sine wave signal C(3θr).
The adder 104 adds the first sine wave signal S(3θr) and a first offset correction value es calculated by the offset correction value calculator 106, to be described hereafter, and adds the second sine wave signal C(3θr) and a second offset correction value ec calculated by the offset correction value calculator 106, to be described hereafter, and outputs the results to the tripled angle calculator 105. The tripled angle calculator 105 carries out an inverse tangent (arctangent) operation on the first sine wave signal to which the first offset correction value es has been added (S(3θr)+es) and the second sine wave signal to which the second offset correction value ec has been added (C(3θr)+ec), and outputs a second tripled angle signal 3θr2, and the second multiplier 107 multiplies the second tripled angle signal 3θr2 by one-third, and outputs the result to the offset angle calculator 108.
The offset angle calculator 108, based on the angle signal θr, offsets the second tripled angle signal 3θr2 multiplied by one-third using the second multiplier 107. Specifically, when value ranges of the angle signal θr are 0 degrees to less than 120 degrees, 120 degrees to less than 240 degrees, and 240 degrees to less than 360 degrees, offset values of the second tripled angle signal 3θr2 multiplied by one-third using the second multiplier 107 are 0 degrees, 120 degrees, and 240 degrees respectively. An output of the offset angle calculator 108 is a calculated angle value θr2.
Continuing, the offset correction value calculator 106 will be described. The offset correction value calculator 106 inputs the second tripled angle signal 3θr2 output from the tripled angle calculator 105, and outputs the first offset correction value es and the second offset correction value ec. Hereafter, an operation of the offset correction value calculator 106 will be described in detail.
The differentiator 106a carries out a differentiating operation with respect to the second tripled angle signal 3θr2, thereby calculating a first speed signal ωr. Herein, s in the drawing is a reference sign representing a Laplacian operator. The low-pass filter 106b outputs a second speed signal ωo wherein a frequency component higher than a time constant T1 has been removed from the first speed signal ωr. The time constant T1 is set to a value that blocks a basic wave frequency of the first sine wave signal S(3θr) of the second tripled angle signal 3θr2. Therefore, the second speed signal ωo is such that a frequency component equal to or higher than the basic wave frequency of the first sine wave signal S(3θr) has been blocked. Herein, the low-pass filter 106b is a primary filter, but provided that the filter is such that a frequency component equal to or higher than the basic wave frequency is blocked, the same advantage is obtained even when a secondary or later filter is adopted.
The first integrator 106c outputs a high cutoff frequency angle signal θ0 obtained by integrating the second speed signal ωo. As the high cutoff frequency angle signal θ0 is obtained by integrating the second speed signal ωo, the high cutoff frequency angle signal θ0 is an angle signal wherein a frequency component equal to or higher than the basic wave frequency of the first sine wave signal S(3θr) has been removed from the second tripled angle signal 3θr2. The subtractor 106d subtracts the high cutoff frequency angle signal θ0 from the second tripled angle signal 3θr2, and calculates an n-fold angle error Δθ wherein a frequency component lower than the basic wave frequency of the first sine wave signal S(3θr) included in the second tripled angle signal 3θr2 has been removed. The gain unit 106e, on inputting the n-fold angle error Δθ, outputs an inverted sign value −Δθ of the angle error, which is the n-fold angle error Δθ multiplied by −1. In the first delayer 106f and the second delayer 106g, z in the drawing represents an operator representing a z-conversion, and the first delayer 106f and the second delayer 106g output a signal input one operating cycle previously.
The first switch 106h has two inputs A and B, outputs the input A (the inverted sign value −Δθ of the n-fold angle error) when it is determined that the high cutoff frequency angle signal θ0 has passed a vicinity of 0 degrees, and outputs the input B (the value of the output of the first switch 106h one operating cycle previously) at other times. Therefore, the first switch 106h outputs an inverted sign value −Δθ0 of the n-fold angle error when the high cutoff frequency angle signal θ0 passes a vicinity of 0 degrees, and this is updated every time the high cutoff frequency angle signal θ0 passes a vicinity of 0 degrees. Also, the second switch 106i has two inputs A and B, outputs the input A (the n-fold angle error Δθ) when it is determined that the high cutoff frequency angle signal θ0 has passed a vicinity of 90 degrees, and outputs the input B (the value of the output of the second switch 106i one operating cycle previously) at other times. Therefore, the second switch 106i outputs an n-fold angle error Δθ90 when the high cutoff frequency angle signal θ0 passes a vicinity of 90 degrees, and this is updated every time the high cutoff frequency angle signal θ0 passes a vicinity of 90 degrees.
The second integrator 106j outputs a value resulting from integrating and outputting the inverted sign value −Δθ0 of the n-fold angle error as an offset correction value of the first sine wave signal S(3θr), that is, the first offset correction value es. In the same way, the third integrator 106k outputs a value resulting from integrating and outputting the n-fold angle error Δθ90 as an offset correction value of the second sine wave signal C(3θr), that is, the second offset correction value ec. Herein, K in the drawing is feedback gain, and by this being regulated, operating responses of the first offset correction value es, which is the offset correction value of the first sine wave signal S(3θr), and the second offset correction value ec, which is the offset correction value of the second sine wave signal C(3θr), are regulated from the second tripled angle signal 3θr2.
Next, advantages of the angle detection device 100A according to the first embodiment will be described in detail. The angle signal θr is expressed in the following Equation (1).
θr=θ+θerr·sin(3θ+β) (1)
Herein, θerr is an amplitude of a component that fluctuates at a frequency three times that of the motor angle of rotation θ included in the angle signal θr. A correction in a case wherein a harmonic (tertiary in this case) component with respect to the motor angle of rotation θ is included in the angle signal θr in this way, as shown in
The angle signal θr is tripled in the first multiplier 101 shown in
3θr=3θ+3θerr·sin(3θ+β) (2)
Herein, as shown in
Next, a sine value (the first sine wave signal S(3θr)) and a cosine value (the second sine wave signal C(3θr)) with respect to the second tripled angle signal 3θr2 are obtained by the sine unit 102 and the cosine unit 103, the first offset correction value es and the second offset correction value ec are added thereto in the adder 104, and the second tripled angle signal 3θr2 is obtained using the tripled angle calculator 105. Herein, when no angle error is included in the first tripled angle signal 3θr, that is, when 3θr coincides with 3θ, an angle difference Δθ1 between the second tripled angle signal 3θr2 and the first tripled angle signal 3θr when the first offset correction value es and the second offset correction value ec are added is as in the following Equation (3).
Δθ1=ec·cos(3θ)−ec·sin(3θ) (3)
Therefore, an angle error synchronous with (having the same cycle as) the first tripled angle signal 3θr can be superimposed on the second tripled angle signal 3θr2, with respect to the first tripled angle signal 3θr, using the first offset correction value es and the second offset correction value ec.
Next, a case wherein the first tripled angle signal 3θr includes an error with respect to the motor angle of rotation θ, as expressed in Equation (2), will be considered. When Equation (2) is expanded, the following Equation (4) results.
3θr=3θ+3θerr·sin(β)·cos(3θ)+3θerr·cos(β)·sin(3θ) (4)
Herein, when defined as in the following equations (5) and (6), Equation (4) becomes the following Equation (7).
θamp_cos=3θerr·sin(β) (5)
θamp_sin=3θerr·cos(β) (6)
3θr=3θ+θamp_cos·cos(3θ)+θamp_sin·sin(3θ) (7)
When the first tripled angle signal 3θr includes an error with respect to the motor angle of rotation θ, as expressed in Equation (2), an angle difference Δθ2, which is a difference between the second tripled angle signal 3θr2 and 3θ, which is a value wherein the motor angle of rotation θ is tripled, is as in the following Equation (8), based on Equations (3) and (7).
Δθ2=(es+θamp_cos)·cos(3θ)+(−ec+θamp_sin)·sin(3θ) (8)
Therefore, Δθ2 is zero when the following Equations (9) and (10) are satisfied.
es=−θamp_cos (9)
ec=θamp_sin (10)
Herein, it is understood from Equations (4) and (5) that θamp_cos is a component synchronous with cos (3θ) of the angle error expressed by the second item on the right side of Equation (2), because of which the component synchronous with cos(3θ) of the angle error can be controlled to zero by calculating the component (a component synchronous with the second sine wave signal C(3θr)), and determining the first offset correction value es, which is the offset correction value of the first sine wave signal S(3θr), so as to satisfy Equation (9).
In the same way, it is understood from Equations (4) and (6) that θamp_sin is a component synchronous with sin (3θ) of the angle error expressed by the second item on the right side of Equation (2), because of which the component synchronous with sin(3θ) of the angle error can be controlled to zero by calculating the component (a component synchronous with the first sine wave signal S(3θr)), and determining the second offset correction value ec, which is the offset correction value of the second sine wave signal C(3θr), so as to satisfy Equation (10).
Therefore, in the first embodiment, the n-fold angle error Δθ, which is the difference between the second tripled angle signal 3θr2 and the high cutoff frequency angle signal θ0, is extracted. Further, as an angle error component is removed by the low-pass filter 106b, the high cutoff frequency angle signal θ0 coincides with triple the motor angle of rotation θ (3θ). Herein, when the extracted n-fold angle error Δθ is given by the following Equation (11), that is, when
Δθ=θ cos 0·cos(θ0)+θ sin 0·sin(θ0) (11),
it is understood from Equation (11) that as the n-fold angle error Δθ when the high cutoff frequency angle signal θ0 is 0 degrees coincides with θ cos 0 when sin (θ0) is 0 and cos (θ0) is 1, the n-fold angle error Δθ (or more precisely the inverted sign value −Δθ of the n-fold angle error) when θ0 is 0 degrees is removed in the first switch 106h, as a result of which −Δθ0 is integrated using the second integrator 106j, and adopted as the first offset correction value es, in order to extract θ cos 0 (a component synchronous with the second sine wave signal C(3θr)) from the n-fold angle error Δθ.
Herein, when looking at the amplitude (es+θamp_cos) relating to cos(3θ) of Equation (8), the amplitude (es+θamp_cos) decreases owing to the first offset correction value es being caused to increase from 0 to a sign differing from that of θamp_cos. Therefore, when θ cos 0 has a positive sign owing to an action of the second integrator 106j, the first offset correction value es decreases, acting in a direction that reduces θ cos 0, and when θ cos 0 has a negative sign, the first offset correction value es increases, acting in a direction that increases θ cos 0. Therefore, θ cos 0 eventually converges on the first offset correction value es, which coincides with 0. Consequently, a component synchronous with cos(θ0) included in the n-fold angle error Δθ converges on zero.
In the same way, it is understood from Equation (11) that as the n-fold angle error Δθ when θ0 is 90 degrees coincides with θ sin 0 when cos(θ0) is 0 and sin(θ0) is 1, the n-fold angle error Δθ when θ0 is 90 degrees is removed in the second switch 106i, as a result of which Δθ90 is integrated using the third integrator 106k, and adopted as the second offset correction value ec, in order to extract θ sin 0 (a component synchronous with the first sine wave signal S(3θr)) from the n-fold angle error Δθ. Herein, when looking at the amplitude (−ec+θamp_sin) relating to sin(3θ) of Equation (8), the amplitude (−ec+θamp_sin) decreases owing to the second offset correction value ec being caused to increase from 0 to θamp_sin, with the same sign. Therefore, owing to an action of the first second integrator 106j, the third integrator 106k acts in a direction that reduces θ cos 0 by increasing the second offset correction value ec when θ cos 0 has a positive sign, and when θ cos 0 has a negative sign, the second offset correction value es decreases, acting in a direction that increases θ cos 0. Therefore, θ sin 0 eventually converges on the second offset correction value ec, which coincides with 0. Consequently, a component synchronous with sin(θ0) included in the n-fold angle error Δθ converges on zero.
As heretofore described, the first offset correction value es and the second offset correction value ec are determined so that the n-fold angle error Δθ converges on zero. The n-fold angle error Δθ converging on zero means that a component fluctuating at a frequency triple that of the motor angle of rotation θ has been removed from the second tripled angle signal 3θr2. Further, by the second tripled angle signal 3θr2 being multiplied in the second multiplier 107, the second tripled angle signal 3θr2 becomes an angle signal (defined as a signal A) that increases from 0 to 120 degrees in a cycle Tc/3, as shown in
According to the angle detection device 100A according to the first embodiment, as heretofore described, an error component fluctuating at a frequency triple that of the motor angle of rotation θ included in the angle signal θr can be removed. Also, an amount of correction is an offset correction value, and regularly an amount of direct current, because of which no error caused by phase deviation occurs, even when there is dead time in calculating the offset correction value. Consequently, a low-priced CPU (central processing unit) with a low operating speed can be used because of the angle detection device 100A according to this embodiment.
In this embodiment, a method whereby an error component fluctuating at a frequency triple that of the motor angle of rotation θ included in the angle signal θr is removed by tripling the angle signal θr has been described, but it goes without saying that a configuration such that an error component fluctuating at a frequency n times that of the motor angle of rotation θ included in the angle signal θr is removed by multiplying the angle signal θr by n (n is a real number other than 1) can be adopted.
Next, an angle detection device according to a second embodiment will be described.
An angle detection device according to the second embodiment is such that only an offset correction value calculator differs from that in the first embodiment, and other portions are the same as in the first embodiment. Consequently, an offset correction value calculator will be described here.
The differentiator 106a, the low-pass filter 106b, the first integrator 106c, and the subtractor 106d have the same functions as in the offset correction value calculator 106 described in the first embodiment. The cosine value calculator 201a calculates the cosine value cos(θ0) with respect to the high cutoff frequency angle signal θ0. In the same way, the sine value calculator 201b calculates the sine value sin(θ0) with respect to the high cutoff frequency angle signal θ0.
Also, the first multiplier 201c multiplies the cosine value cos(θ0) and the n-fold angle error Δθ, thereby calculating Δθ cos(θ0). In the same way, the second multiplier 201d multiplies the sine value sin(θ0) and the n-fold angle error Δθ, thereby calculating Δθ sin(θ0). The second integrator 201e carries out an operation of the following equation (12) with respect to Δθ cos(θ0), thereby calculating a cosine component θ1f_cos_amp of the high cutoff frequency angle signal θ0 of the inverted sign value −Δθ of the n-fold angle error. Herein, T2 is a cycle of the second tripled angle signal 3θr2.
In the same way, the third integrator 201f carries out an operation of the following equation (13) with respect to Δθ sin(θ0), thereby calculating a sine component θ1f_sin_amp of the high cutoff frequency angle signal θ0 of the n-fold angle error Δθ. Herein, the cycle T2 of the second tripled angle signal 3θr2 is of the same value as in Equation (7).
Further, the second integrator 201e inputs the cosine component θ1f_cos_amp of the inverted sign value −Δθ of the n-fold angle error into the fourth integrator 201g, and the third integrator 201f inputs the sine component θ1f_sin_amp of the n-fold angle error Δθ into the fifth integrator 201h. The fourth integrator 201g integrates θ1f_cos_amp, and outputs a value thereof as the first offset correction value es. In the same way, the fifth integrator 201h integrates θ1f_sin_amp, and outputs a value thereof as the second offset correction value ec. Herein, K is feedback gain, and it is sufficient that this is determined in the same way as in the first embodiment.
Next, advantages of the angle detection device according to the second embodiment will be described.
In the first embodiment, a case wherein the angle signal θr is expressed by Equation (1) has been considered, but in actuality, there are also cases wherein a component of another order is included. For example, a case wherein the angle signal θr is such that an amplitude θerr2 of a component that fluctuates at a frequency twice that of the motor angle of rotation θ is included in the angle signal θr will be considered with respect to Equation (1), as shown in the following Equation (14).
θr=θ+θerr·sin(3θ+β)+θerr2·sin(2θ+γ) (14)
In this case, when attempting to obtain the high cutoff frequency angle signal θ0 using the subtractor 106d of the offset correction value calculator 106 in the first embodiment shown in
As heretofore described, the angle detection device according to the second embodiment is such that an unprecedented, notable advantage is achieved in that an angle error can be correctly extracted and reduced, even when a component other than a component to be extracted and reduced is included in an angle error existing with respect to the motor angle of rotation θ included in the angle signal θr.
Next, an angle detection device according to a third embodiment will be described.
An angle detection device according to the third embodiment is such that only an offset correction value calculator differs from that described in the second embodiment, and other portions are the same as in the first embodiment or the second embodiment. Consequently, an offset correction value calculator will be described here.
The third switch 301a and the fourth switch 301c have two inputs A and B, output the input A when it is determined that the second speed signal ωo is higher than the preset reference speed ω, and output the input B at other times. z shown in the third delayer 301b and the fourth delayer 301d is an operator representing a z-conversion, and the third delayer 301b and the fourth delayer 301d output an input signal of the offset correction value calculator 301 one operating cycle previously as an output signal.
Therefore, the third switch 301a outputs the input A, which is the output of the fourth integrator 201g, when it is determined that the second speed signal co is higher than the preset reference speed ω, and when this is not the case, the third switch 301a outputs the input B, which is the offset correction value es of one operating cycle previously. Therefore, the third switch 301a updates the offset correction value es when the second speed signal ωo is higher than the reference speed ω. In the same way, the fourth switch 301c outputs the input A, which is the output of the fifth integrator 201h, when it is determined that the second speed signal ωo is higher than the preset reference speed ω, and when this is not the case, the fourth switch 301c outputs the input B, which is the offset correction value ec of one operating cycle previously. Therefore, the fourth switch 301c updates the offset correction value ec when the second speed signal ωo is higher than the reference speed ω.
By a calculation of an offset correction value being carried out when the second speed signal ωo is higher than the reference speed co in this way, an error occurring in the offset correction value due to interference between a frequency of an angle error to be extracted and reduced and a rotating machine speed change frequency can be removed.
In particular, when the rotating machine is a motor for electric power steering, correction using an offset correction value can be effectively carried out by the reference speed co being set to a speed higher than a driver's steering wheel manipulation frequency.
Also, a number of calculations per rotation of the rotating machine decreases as the speed of the rotating machine increases, because of which offset correction value calculation accuracy decreases. Therefore, the third switch 301a, the fourth switch 301c, the third delayer 301b, and the fourth delayer 301d are provided, the input A is output from the third switch 301a and the fourth switch 301c when it is determined that the speed of the rotating machine is lower than the preset reference speed ω, and the input B is output at other times, whereby a setting can also be such that an offset correction value calculation is carried out when the speed of the rotating machine is equal to or lower than a predetermined value.
Next, an angle detection device according to a fourth embodiment will be described.
In
For example, when the angle signal θr output from the angle calculator 9 is expressed by Equation (13), an offset correction using the first sine wave signal S(3θr) and the second sine wave signal C(3θr) that are twice the angle signal θr is carried out in the first angle corrector 10a, whereby a component that fluctuates at a frequency twice that of the motor angle of rotation θ is extracted, and a reduced angle signal θr3 is calculated.
Also, an offset correction using a third sine wave signal and a fourth sine wave signal, wherein the angle signal θr is tripled, is carried out in the second angle corrector 10b, and a detected angle value θr2 from which a component that fluctuates at a frequency triple that of the motor angle of rotation θ has been extracted and removed is extracted.
A multiple of angle correctors (10a and 10b) being connected in series with respect to the angle signal θr, and the output thereof being adopted as the detected angle value θr2 in this way, means that even when multiple angle error components exist in the angle signal θr, the multiple of components can be extracted and removed.
Also, an offset correction calculator of the first angle corrector 10a and an offset correction calculator of the second angle corrector 10b being of the same configuration means that although inputs and outputs differ, calculations can be carried out using the same function, because of which an increase in a ROM (read-only memory) size can be restricted.
Herein, with regard to an order in which the multiple of angle correctors are caused to operate, operation is preferably started from the component of the lowest order (lowest frequency) of the angle error to be corrected. Therefore, when correcting m1 (m1 is a real number) and m2 (a real number satisfying m2>m1) components of an angle signal, the angle corrector relating to m1 is caused to operate first, after which the angle corrector relating to m2 is caused to operate. By so doing, an advantage is achieved in that extraction of the n-fold angle error Δθ caused by a difference with respect to the high cutoff frequency angle signal θ0 can be carried out more accurately and in a high-speed region. In this embodiment, two angle correctors (10a and 10b) are connected in series, but it goes without saying that three or more angle correctors may be connected in series.
Next, an electric power steering device in which the angle detection device of any one of the first to fourth embodiments is used will be described as a fifth embodiment.
Although the angle detection devices 100A and 100B have been described in the first to fourth embodiments, an electric power steering device wherein torque that assists steering torque is generated based on the detected angle value θr2 obtained using the angle detection device 100A or 100B may also be configured.
In
A driver carries out steering of the front wheel 406 by causing the steering wheel 403 to rotate left and right. The torque detector 404 detects a steering torque Ts of a steering system, and outputs the detected torque to the assist torque calculator 402. In the voltage command generator 401, a voltage V is applied to the alternating current motor 407 based on the detected angle value θr2 and the steering torque Ts, and the alternating current motor 407 generates torque that assists the steering torque Ts via the gear 405.
The resolver 1 detects an angle of rotation θ of the alternating current motor 407. In the voltage command generator 401, it is sufficient that a current command value of the alternating current motor 407 is calculated based on, for example, the steering torque Ts, a voltage command is calculated using the current command value and the detected angle value θr2, and the voltage V is applied to the alternating current motor 407 using a power converter, such as an inverter, that has the calculated voltage command as an input. Alternatively, publicly known technology, such as separately providing a current detector that detects the current of the alternating current motor 407, and calculating a voltage command value based on a deviation between a current command value and the current flowing through the alternating current motor 407 detected by the current detector, may be used.
This kind of electric power steering device is such that accuracy of the detected angle value θr2 with respect to the angle of rotation θ of the alternating current motor 407 is important. For example, when an angle error with respect to the angle of rotation θ of the alternating current motor 407 occurs in the detected angle value θr2, the voltage command generator 401, based on this, applies the voltage V including the angle error, because of which a problem occurs in that torque ripple, vibration, abnormal noise, or the like, emanating from the alternating current motor 407 occurs. For the heretofore described reason, the electric power steering device is such that accuracy of the detected angle value θr2 with respect to the angle of rotation θ of the alternating current motor 407 is extremely important.
The electric power steering device according to the fifth embodiment is such that the angle signal θr output from the angle calculator 9 is corrected to the detected angle value θr2 and output using the angle corrector 10, because of which advantages are obtained in that an angle error is restricted, and a quiet electric power steering device can be constructed.
Examples wherein the resolver 1 is used as an angle detector have been described in the first to fifth embodiments, but it goes without saying that the same advantages are obtained when using an angle detector that outputs a sine signal and a cosine signal with respect to a motor angle of rotation, for example, an MR sensor or an encoder.
Also, examples wherein a motor angle of rotation is detected as an angle detection target have been described in the first to fifth embodiments, but it goes without saying that the same advantages are obtained when an angle of rotation of a rotating body other than a motor is detected.
Although the present application is described in terms of various exemplifying embodiments and implementations, the various features, aspects, and functions described in one or a multiple of the embodiments are not limited in their applicability to a particular embodiment, but instead can be applied, alone or in various combinations, to other embodiments.
It is therefore understood that numerous modifications that have not been exemplified can be devised without departing from the scope of the present application. For example, at least one constituent component may be modified, added, or eliminated, and furthermore, at least one constituent component may be extracted and combined with the constituent components of another embodiment.
1 resolver, 2 excitation circuit, 3 differential amplifier, 4a, 4b angle calculating means, 5 excitation coil, 6 sine detecting coil, 7 cosine detecting coil, 8 A/D converter, 9 angle calculator, 10 angle corrector, 10a first angle corrector, 10b second angle corrector, 100A, 100B angle detection device, 101, 201c first multiplier, 102 sine unit, 103 cosine unit, 104 adder, 105 tripled angle calculator, 106, 201, 301 offset correction value calculator, 106a differentiator, 106b low-pass filter, 106c first integrator, 106d subtractor, 106e gain unit, 106f first delayer, 106g second delayer, 106h first switch, 106i second switch, 106j, 201e second integrator, 106k, 201f third integrator, 107, 201d second multiplier, 108 offset angle calculator, 201a cosine value calculator, 201b sine value calculator, 201g fourth integrator, 201h fifth integrator, 301a third switch, 301b third delayer, 301c fourth switch, 301d fourth delayer, 401 voltage command generator, 402 assist torque calculator, 403 steering wheel, 404 torque detector, 405 gear, 406 front wheel, 407 alternating current motor, P processor, M storage device, es first offset correction value, ec second offset correction value, S(θ) sine signal, C(θ) cosine signal, θ angle of rotation, θr, θr3 angle signal, θr2 detected angle value, 3θr first tripled angle signal, S(3θr) first sine wave signal, C(3θr) second sine wave signal, 3θr2 second tripled angle signal, ωr first speed signal, coo second speed signal, co reference speed, θ0 high cutoff frequency angle signal, Δθ n-fold angle error, θoffset offset angle, Ts steering torque.
Filing Document | Filing Date | Country | Kind |
---|---|---|---|
PCT/JP2018/046482 | 12/18/2018 | WO |
Publishing Document | Publishing Date | Country | Kind |
---|---|---|---|
WO2020/129144 | 6/25/2020 | WO | A |
Number | Name | Date | Kind |
---|---|---|---|
20140316733 | Mori | Oct 2014 | A1 |
20140354271 | Kawase | Dec 2014 | A1 |
Number | Date | Country |
---|---|---|
2008-273478 | Nov 2008 | JP |
2009-014358 | Jan 2009 | JP |
2015-132593 | Jul 2015 | JP |
2015132593 | Jul 2015 | JP |
5762622 | Aug 2015 | JP |
2013136612 | Sep 2013 | WO |
WO-2013136612 | Sep 2013 | WO |
Entry |
---|
Communication dated Jan. 5, 2022 from the Japanese Patent Office in Application No. 2020-560670. |
International Search Report for PCT/JP2018/046482 dated Mar. 12, 2019. |
Number | Date | Country | |
---|---|---|---|
20210323603 A1 | Oct 2021 | US |