• 专利附录
  • 专利说明
  • 权利要求
  • 类似技术
  • 同族专利
  • 引用文献
  • 法律状态
  • 优先权
    • 专利摘要:
    The present invention relates to a method for determining the position 0 of a moving part (T) along an axis (X) with the aid of an inductive sensor (10) comprising: • a primary winding ( B1) generator of an electromagnetic field, • a first secondary winding (R1), generating a first voltage signal (V1), of sinus function type, • a second secondary winding (R2), generating a second voltage signal (V2 ) of the cosine function type • a calculation unit (20 '), the method of the invention comprising steps for calculating and distributing linearization points i on the tangent arc function tan (θ), resulting from the ratio of the first signal voltage on the second voltage signal, the linearization points i being distributed according to a sinusoidal function in order to reduce the error on the position (θ) of the target (T) at the ends (E1, E2) of the primary and secondary windings (R1, R2).
    公开号:FR3036790A1
    申请号:FR1554773
    申请日:2015-05-27
    公开日:2016-12-02
    发明作者:Olivier Gerardiere；Jeremie Blanc；Jean-Louis Roux
    申请人:Continental Automotive GmbH；Continental Automotive France SAS；
    IPC主号:
    专利说明:

    [0001] The present invention relates to a method for determining the position of a target along an axis using an inductive position sensor. This type of sensor has the advantage of making it possible to determine the position of a mechanical part, or of any other element, without requiring contact with the part whose position one wishes to know. This advantage makes the applications of such sensors are very numerous in all types of industries. Such sensors are also used in consumer applications such as the automotive field in which the present invention has been made. However, it can be used in other diverse and varied fields.
    [0002] The operating principle of an inductive sensor is based on the coupling variation between a primary winding and secondary windings of a transformer operating at high frequency and without using a magnetic circuit. The coupling between these windings varies according to the position of a moving conductive part (electricity), generally called "target". Currents induced in the target indeed change the currents induced in the secondary windings. By adapting the configuration of the windings and knowing the current injected into the primary winding, the measurement of the current induced in the secondary windings makes it possible to determine the position of the target. To integrate such an inductive sensor in a device, in particular an electronic device, it is known to make the transformer mentioned above on a printed circuit board. The primary winding and the secondary windings then consist of tracks traced on the printed circuit board. The primary winding is then for example powered by an external source and the secondary windings are then the seat of currents induced by the magnetic field created by the flow of a current in the primary winding. The target, which is a conductive part, for example metallic, may have a simple shape. It may for example be a piece cut from a sheet. To produce a linear sensor, the cut-out for producing the target is, for example, rectangular whereas for a rotary sensor, this cut-out will for example be in the form of an angular sector of radius and angle adapted to the movement of the part. In FIG. 3, the inductive sensor 10 is represented, comprising inter alia: a primary winding B1 exciter, and two secondary windings Ri, R2 receivers. The target T moves along the inductive sensor, along an axis X, modifying the currents (eddy currents) in the secondary windings Ri, R2, which are induced by the electromagnetic flux generated by the primary winding B1. Generally, two sets of secondary windings R1, R2 are designed to perform on a complete stroke of the inductive sensor 10 respectively sine and cosine functions of the position of the target T. The first and second secondary windings R1, R2 generate at their terminals 5 a first voltage signal V1 and a second voltage signal V2, of sinus and cosine form (see FIG. 1) as a function of a spatial angle θ, representative of the position of the target T along the axis X. Such functions (cosine and sine) are well known and can easily be processed by a control unit 20, integrated in an electronic system, / 0 shown schematically in FIG. 3. By making the ratio of the sine by the cosine then by applying a tangent arc function, an image of the position of the target T along the X axis is obtained (see Figure 2). This is illustrated in FIG. 2, which represents the tangent arc function "tan" as a function of the position P of the target T. The argument of the sine and cosine functions is a linear (or affine) function of the position of the target T whose race then represents a greater or lesser part of the spatial period of these trigonometric functions. As illustrated in FIG. 2, the tangent arc function thus obtained is not strictly linear. In order to obtain a direct relationship between the tangent arc function and the position of the target T along the axis, for example at spatial angle θ, it is known from the prior art to linearize the tangent arc function. For this purpose, a linear regression y = ax + b, that is, y = axO + b, where a and b are two constants, is applied to the tangent arc function. Said linear regression is applied to consecutive segments of values of said function, spaced apart by spacial pitch of step 3.0 which are identical to each other and equidistant (see FIG. This linear regression is known to those skilled in the art. For each segment 3.0, we apply the linear interpolation y = axO + b. This is known to those skilled in the art. A straight linear regression line DL is thus obtained, allowing for each value of the tangent arc function to directly know the position 0 of the target T. However, the linearization of the tangent arc function induces an inaccuracy at the E1, E2 ends of the race C of the target (see Figure 2), where there are significant edge effects. This lack of linearity impacts the accuracy of the position P of the target T at these ends E1, E2.
    [0003] As illustrated in FIG. 1, at each end E1, E2, a notable difference 3.1, 32 exists between the actual position 0 of the target T and that indicated by the line DL.
    [0004] These inaccuracies at the ends E1, E2 reduce the useful travel Cu of the target T to approximately 60% of the length L of the two secondary coils R1, R2 (see FIG. this problem and proposes a method of determining the position of a target T along an axis using an inductive position sensor making it possible to reduce the inaccuracy on the position of the target T at the ends E1, E2 of the race Cu of said target T and therefore to lengthen the useful stroke Cu of the target with respect to the prior art.The invention proposes a method for determining the position of a moving part, called "target", the along an axis, using an inductive sensor, said inductive sensor comprising: - a primary winding generating an electromagnetic field, - a first secondary winding, generating a first voltage signal, of the sinus function type, representative of the current induced in said p first secondary winding, when the target moves in front of the first secondary winding, - a second secondary winding, generating a second cosine function voltage signal representative of the current induced in said second secondary winding, when the target moves in front of the second winding. second secondary winding, - a calculation unit, said determination method according to the invention comprising the following steps: - Step 1: calculation of a tangent arc function from the first voltage signal and the second voltage signal, 25 - Step 2: calculation of an error between the tangent arc function thus calculated and a predetermined straight line, - Step 3: calculation of the positions of linearization points of the tangent arc function according to the formula Ot = (i-1) x) [sin (1) x12) XF x Cul (n-1 with index of linearization points varying from 1 to n, Ot: position of linearization point i at spatial angle, F: spacing factor of p linearization anoints, with F> 0 and FmAx such that: ((i-1) x2xn. x MAX (i-1) X-1) Cu [Sill (n-1) 35 Cu: useful sensor stroke along the spatial angle axis. Step 4: for each value of the tangent arc function, search for an index i of the linearization point such that: Oi <O <ei + i with: 5 0: position of linearization point i at spatial angle, position of the linearization point (i +1) at spatial angle, 0: spatial angle. Step 5: calculation of a correction to be applied to the tangent arc function according to the formula: Corr (tan (0)) = tan (9) -tan (9) with: Corr (tan (0)): correction on arc function tangent to spatial angle 0, spatial angle error 0, spatial angle error 0i + 1, 15 tan (01): arc function value tangent to spatial angle 0, tan ( Oi + i): value of the arc function tangent to the spatial angle 0, tan (0): value of the arc function tangent to the spatial angle 0. - Step 6: calculation of a corrected tangent arc function: tan rr (0) = tan (0) + Corr (tan (0)) 20 with: tancorr (0): corrected tangent arc function, tan (0): arc tangent function, Corr (tan (0)): correction on the arc function tangent to the spatial angle θ. - Step 7: determination of the position of the target along the axis from the tangent arc function thus corrected. Preferably, during step 2, the predetermined straight line consists of a linear regression of the tangent arc function. The invention also relates to an inductive sensor for the position of a target along an axis comprising: a primary winding generating an electromagnetic field; a first secondary winding generating a first voltage signal of a function type sinus, representative of the current induced in said first secondary winding, when the target moves in front of the first secondary winding, E (01) [E (011) - E (01)] X [tan (ei + i) -tan (ei A second secondary winding, generating a second cosine-function-type voltage signal, representative of the current induced in said second secondary winding, when the target moves in front of the second secondary winding, a computing unit, according to FIG. invention the calculation unit comprises: first means for calculating the tangent arc function from the first voltage signal and the second voltage signal; second means for calculating an error between the arc function; a tangent thus calculated and a predetermined straight line; third means for calculating the position of linearization points of the tangent arc function (according to the formula: Ot = (i -1) x [sin (1) x12) "(n- 1) XF x Cu] with: 15 i: linearization point index varying from 1 to n, Oi: position of linearization point i at spatial angle, F: spacing factor of linearization points, with F> 0 and FmAx such that: ((i-1) x2x) X Cu FMAX <(i - 1) x - (n-1) Cu [n.Sirl (n-1) Cu: useful stroke of the sensor along the axis in spatial angle. Means for searching for a linearization point index i such that, for each value of the tangent arc function: Oi <O <0t + with: 0: position of the linearization point i at a spatial angle, 25 0i + 1 : position of the linearization point (i +1) at spatial angle, 0: spatial angle. the fourth means for calculating the correction to be applied to the tangent arc function according to the formula: (i) Corr (tan (0)) = E (i) + [E (i + 1) - E (0 rtan (60 -tan 1 x Ltan (i + 1) -tan (i)] 30 with: Corr (tan (0)): correction on the arc function tangent to the spatial angle 0, E (i): error at the point of linearization E (i + 1): error at the linearization point (i + 1), tan (i): value of the tangent arc function at point i, 35 tan (i + 1): value of the arc function tangent to the point ( i + 1), 3036790 6 tan (0): value of the arc function tangent to the spatial angle 0. - fifth means of calculating the corrected tangent arc function: tan '' (0) = tan (0) + Corr (tan (0)) with: 5 tan'rr (0): corrected tangent arc function, tan (0): tangent arc function, Corr (tan (0)): correction on arc function tangent to spatial angle 0. - means for determining the position of the target along the axis from the tangent arc function thus corrected. / 0 The invention applies equally any motor vehicle comprising an inductive sensor according to the characteristics listed above. Other features and advantages of the invention will become apparent on reading the following description and on examining the appended drawings in which: FIG. 1, explained above, represents, according to the spatial angle θ, the first signal of voltage V1 and the second voltage signal V2 respectively at the terminals of the first secondary winding R-1 and the second secondary winding R2 respectively, FIG. 2, explained above, represents the tangent arc function according to the position P of the target T along the X axis, FIG. 3, explained above, represents the inductive sensor 10 of the prior art, FIG. 4 schematically represents the error on the tangent arc function with respect to the linear regression line DL, in function of the spatial angle θ, FIG. 5 diagrammatically represents the distribution of the linearization points according to the invention as a function of the spatial angle θ, FIG. corrected angente according to the invention, FIG. 7 diagrammatically represents the calculation unit 20 'according to the invention.
    [0005] As illustrated in FIG. 2, and previously explained, the position inductive sensor 10, which makes it possible to measure the position of a target T moving along an axis X, comprises: a primary winding B1 generating a field electromagnetic, - a first secondary winding Ri, generating a first voltage signal V1 as a function of a spatial angle θ (see FIG. 1), of sinus function type, representative of the current induced in said first secondary winding R1, when the target T moves in front of the first secondary winding, along the X axis, - a second secondary winding R2, generating a second voltage signal V2 as a function of a spatial angle θ (see FIG. cosine, representative of the current induced in said second secondary winding R2, when the target T moves in front of the second secondary winding, along the axis X, - a computing unit 20, which supplies voltage to the primary winding Bi, and which m is the first voltage signal V1, and the second voltage signal V2 respectively at the terminals of the first secondary winding R1 and at the terminals of the second secondary winding R2 to derive the position of the target T along the X axis For the sake of clarity, the position of the target T along the X axis will here be expressed in spatial angle 0. It should be noted that the invention applies similarly to determine the position of the target. T along the X axis, expressed in x (cm or mm) distance. According to the prior art, in order to determine the position of the target T along the X axis, it is known to calculate the tangent arc of the ratio between the sine and the cosine, i.e. say between the first voltage signal V1 and the second voltage signal V2, oinsee either: tan (0) = () = (vi2), then linearize the tangent arc function thus obtained, by applying a linear regression of the type y = ax0 + b, on segments of values of said function, spaced from spatial angle 3.0 identical to each other and equidistant (see Figure 2).
    [0006] However, this method of determining the position of the target T according to the prior art does not make it possible to determine accurately the position of the target T at the ends E1, E2 of the total path of the target T, that is, that is to say at the ends E1, E2 of the secondary coils R1, R2. This disadvantage has the consequence of significantly reducing the useful travel Cu of the target T. In order to overcome this drawback, the invention proposes the following method for determining the position of the target T, explained below. In a first step (step 1), the tangent arc function tan (0) is calculated, as in the method of determining the prior art, such that: sine tanw = (_ = (1l1 cos 9) Ii2) 35 with : 3036790 8 V1: first voltage signal, representative of the sine function, V2: second voltage signal representative of the cosine function. In a second step (step 2), according to the invention, an error E (0) between the arctangent function tan (0) and a predetermined line DL (see FIG. 4) is calculated.
    [0007] 5 E (0) = tan (0) - DL In a preferred embodiment, said line DL is the linear regression of the tangent arc function and has the equation yDL = y = axO-Eb (see FIG. E (0) = tan (0) - yDL The said error E (0) is illustrated in FIG. 4 and is larger at the ends E1, E2 of the race of the target T. In a third step (step 3), the position of linearization points i (i.e., linear regression) of tangent arc function tan (0), according to spatial angle θ are calculated according to the equation: θ 0 = (i -1) x (ncui) [sin ((i-1) x2xn.) XF x Cul [1] (n-1) with: 0 position of linearization point i at spatial angle 0, linearization point index varying from 1 to n in this example, n is between 5 and 101. It should be noted that n may be greater than 101.
    [0008] F: spacing factor of linearization points i with F> 0 and FmAx such that: ((i-1) x2x ass MAX (i - 1) X - (n-1) Cu [n.Sirl (n- 1) Cu: Useful travel of the sensor 10 along the X axis at a spatial angle θ of between 00 and 360 ° n-: constant equal to 3.14.
    [0009] The invention resides in the use of a sinusoidal function in order to distribute the linear regression points i on the tangent arc function tan (0). The distribution of the linear regression points i according to the sinusoidal function makes it possible to densify the number of linearization points i at the ends E1, E2 of the tangent arc function, where the error E (0) is the largest (see FIG. 4).
    [0010] It should be noted that the invention can be realized by using the tangent arc function instead of the sine function in equation [1]. In FIG. 4, 9 linear regression points i, that is to say n = 9, are illustrated. At the end E1, the first three linearization points 0, 1, 2 and at the E2 end are illustrated. , are the last three linearization points 7, 8, 9.
    [0011] The distribution of the points 0, 1, 2, 7, 8, 9 at the ends E1, E2 is denser than that of the points 4, 5, 6 over the remainder of the useful stroke Cu of the target T.
    [0012] In a fourth step (step 4), for each value of the tangent arc function tan (0), the window of linear regression points i in which the abscissa 0 of said value is determined. More precisely for each value tan (0), the index i of the linearization point is determined such that: with: Oi: position of linearization point i at spatial angle, position of linearization point (i + 1) at angle spatial, 0: spatial angle.
    [0013] An example is illustrated in FIG. 5. In this example, the value tan (0) corresponds to a spatial angle θ included in the window of points i = 7 and (i + 1) = 8 of linear regression. In step 5, the correction to be applied to the tangent arc function tan (0) is calculated according to the following formula: (0i) 15 Corr (tan (0)) = "'rE (0-E`0 + ( ) 1 i '' e + 1e- X [tan (60-tantan (ei + i) -tan (ei) -1 with: Corr (tan (0)): correction on the arc function tangent to the spatial angle 0 , spatial angle error Oi, spatial angle error 0i + 1, 20 tan (01): value of the arc function tangent to the spatial angle 0, tan (Oi + i): value of the arc function tangent to the spatial angle 0, tan (0): value of the arc function tangent to the spatial angle 0. Then, in the sixth step, (step 6), the correction thus calculated is applied to the tangent arc function tan (0) 25 tan'rr (0) = tan (0) + Corr (tan (0)) with: tan'rr (0): corrected tangent arc function, tan (0): arc tangent function, Corr (tan (0)): correction on the arc function tangent to the spatial angle 0.
    [0014] This is illustrated in FIG. 6, the thus corrected tangent arc function tan'rr (0) is a straight line, different from the linear regression line DL of the prior art. Said corrected tangent arc function has at its ends El, E2, errors 31 'and 32 between said corrected function tan'rr (0) and the tangent arc function tan (0) less than the errors 31 and 32 between the arc function tangent tan (0) and the linear regression line DL of the prior art.
    [0015] Thanks to the precision provided by the method for determining the invention at the ends E1, E2, the useful stroke Cu of the target T is then significantly increased. The new useful stroke Cd obtained by the determination method according to the invention is approximately 20% longer than the useful stroke Cu of the prior art, for example with the linearization method according to the prior art. , the useful stroke Cu is equal to 40 mm, and according to the method of the invention, the new useful stroke Cu '= 48 mm Steps 1 to 7 can be performed in software, by an electronic computer electrically connected to the sensor 10, or alternatively, by the computing unit 20 'according to the invention (see FIG. 7) The invention also relates to an inductive position sensor 10 comprising: a primary winding B1 generating an electromagnetic field, a first secondary winding R1, generating a first voltage signal V1, of the sinus function type, a second secondary winding R2, generating a second voltage signal of the cosine function type, a calculation unit 20 ', invent i, the computing unit 20 'is adapted to perform steps 1 to 7 of the determination method detailed above.
    [0016] For this purpose, the computing unit 20 'according to the invention comprises (see FIG. 7): first calculation means (M1) of the tangent arc function tan (0) from the first voltage signal V1 and the second voltage signal V2, - second calculation means (M2) of an error E (0) between the thus calculated tangent arc function tan (0) and a predetermined line DL, in the preferred embodiment of the invention, the predetermined straight line DL is the linear regression line of said tangent arc function tan (0), - third calculation means (M3) of the position of linear regression points of the tangent arc function according to the formula: Ot = (i - 1) x C-5 [sin (1) x12) "XF x Cul (n-1 with: Ot: position of linearization point i at spatial angle 0, linearization point index varying from 1 to n, in this example, n is between 5 and 101.
    [0017] 3036790 11 F: spacing factor of linearization points i, with F> 0 and FmAx such that: ((i-1) x2xn x x MAX MAX G (i - 1) X Cu [Sirl (n-1) Cu : useful stroke of the sensor 10 along the X axis at a spatial angle θ, ranging between 00 and 360 °, rt: constant equal to 3.14, - search means (MR) of the index i of the point of linearization, for each value of the tangent arc function, such that: Oi <O <ei + i 10 with: Oi: position of the linearization point i at spatial angle, Ot + 1: position of the linearization point (i +1 ) at spatial angle, 0: spatial angle - fourth calculation means (M4) of the correction to be applied to the tangent arc function according to the formula: Corr (tan (0)) = E (0,) + [E (0) tan (9 / + 1) -tan (9 / E (e) ix Ltane-t-1) with: Corr (tan (0)): correction on the arc function tangent to the spatial angle 0, 20 E (01): error at the spatial angle Oi, error at the spatial angle Ot + i, tan (01): value of the arc function tangent to the spatial angle Oi, tan (Oi + i): value of the arc function tangent to the spatial angle Ot + i, tan (0): value of the arc function tangent to the spatial angle θ. - the fifth calculation means (M5) of the corrected tangent arc function: tan ' , (0) = tan (0) + Corr (tan (0)) with: tan'rr (è): corrected tangent arc function, 30 tan (0): arc tangent function, Corr (tan (0)): correction on the arc function tangent to the spatial angle 0. - determination means (MD) of the position 0 of the target T along the X axis from the tangent arc function thus corrected tan'rr (0) .
    [0018] The first, second, third, fourth, fifth calculation means, the search means and the determination means, M1, M2, M3, M4, M5, MR, MD, are in the form of integrated software in the form of softwares. the calculation unit 20 '(see FIG.
    [0019] The invention resides in a judicious correction of the tangent arc function, which is performed by inexpensive software means. The invention therefore makes it possible to considerably extend the useful travel of an inductive position sensor by improving the accuracy of the position of the target at the ends of the race.
    权利要求:
    Claims (4)
    [0001]
    REVENDICATIONS1. A method for determining the position of a moving part, called a "target" (T), along an axis (X), using an inductive sensor (10), said inductive sensor (10) comprising a primary winding (B1) generating an electromagnetic field, a first secondary winding (R1), generating a first voltage signal (V1), of the sinus function type, representative of the current induced in said first secondary winding (R1). ), when the target (T) moves in front of the first secondary winding (R1), - a second secondary winding (R2), generating a second voltage signal (V2) of the cosine function type, representative of the current induced in said second winding secondary (R2), when the target moves in front of the second secondary winding (R2), - a calculation unit (20 '), said determination method being characterized in that it comprises the following steps: - Step 1: calculation of a tangent arc function (tan (0)) from the p first voltage signal (V1) and the second voltage signal (V2), - Step 2: calculation of an error (E (0)) between the tangent arc function (tan (0)) thus calculated and a predetermined line ( DL), 20 - Step 3: calculation of the positions of linearization points (and) of the tangent arc function (tan (0)) according to the formula and = (i-1) x) [sin (1) x12) "XF x Cul (n-1 with: index of linearization points ranging from 1 to n, 25 Ot: position of linearization point i at spatial angle, F: spacing factor of linearization points, with F> 0 and FmAx tel that: ((i-1) x2xn. x cul MAX (i - 1) X (n-1) Cu [sin (n-1) Cu: useful stroke of the sensor along the axis in spatial angle. 3036790 14 - Step 4: for each value of the tangent arc function (tan (0)), search for an index (i) of a linearization point such that: Oi <O <0t + with: 5 0: position of the linearization point i at spatial angle, linearization point position (i +1) at spatial angle, 0: spatial angle. Step 5: calculation of a correction to be applied to the tangent arc function (tan (0)) according to the formula: Corr (tan (0)) = (0) + [E (01 + 1) E (01) ] x [tatnan (e (i92:) - tatnan (e (ie) i) J1 with: Corr (tan (0)): correction on arc function tangent to spatial angle 0, spatial angle error 0 , E (01 + 1): error at the spatial angle 0i + 1, tan (01): value of the arc function tangent to the spatial angle 0, tan (Oi + i): value of the arc function tangent to the spatial angle tan (0): value of the arc function tangent to the spatial angle 0. - Step 6: calculation of a corrected tangent arc function (tan'rr (0)): tan ', (0) = tan (0) + Corr (tan (0)) with: tan'rr (0): corrected tangent arc function, tan (0): tangent arc function, Corr (tan (0)): correction on the arc function tangent to the spatial angle 0. - Step 7: determination of the position (0) of the target (T) along the axis (X) from the tangent arc function thus corrected (tan'rr (0)).
    [0002]
    2. Determination method according to the preceding claim, characterized in that in step 2 the predetermined straight line (DL) consists of a linear regression (yin) of the tangent arc function (tan (0)).
    [0003]
    An inductive position sensor (10) of a target (T) along an axis (X) comprising: a primary winding (B1) generating an electromagnetic field, a first secondary winding ( R1), generating a first sinus function-type voltage signal (V1) representative of the current induced in said first secondary winding (R1), when the target moves in front of the first secondary winding (R1), - a second winding secondary signal (R2), generating a second voltage signal (V2) of the cosine function type, representative of the current induced in said second secondary winding (R2), when the target moves in front of the second secondary winding (R2), / 0 - a calculation unit (20 '), characterized in that the computing unit (20') comprises: - first calculation means (M1) of a tangent arc function (tan (0)) from the first signal of voltage (V1) and the second voltage signal (V2), - the second calculation means (M2) of an error (E (0)) between the tangent arc function (tan (0)) thus calculated and a predetermined straight line (DL), - the third calculation means (M3) of the linearization point positions (Oi) of the function arc tangent (tan (0)) according to the formula: and = (i-1) x [sin ((i (n-1) x12) ") XF x Cul (n-1) with: index of linearization point varying from 1 to n, Oi: position of linearization point i at spatial angle, F: linearization point spacing factor, with F> 0 and FmAx such that: ((i-1) x2xn. x Fm Ax (i-1) x (n-1) Cu [sin (n-1) Cu: useful stroke of the sensor along the spatial angle axis. search means (MR) of an index (i) of linearization point such that, for each value of the tangent arc function: oi <O <0i-Fi with: 0: position of linearization point i at angle spatial, 3036790 16 position of the linearization point (i +1) at spatial angle, 0: spatial angle. fourth means for calculating (M4) a correction to be applied to the tangent arc function according to the formula: 5 = E (i) [E (i + 1) _ E (i), r tan (6) -tan (i) Corr (tan (0)) Ltan (i + 1) -tan (i)] with: Corr (tan (0)): correction on the arc function tangent to the spatial angle 0, E (i): error at the linearization point E (i + 1): linearization point error (i + 1), tan (i): value of the arc function tangent at point i, tan (i + 1): value of the function arc tangent to the point (i + 1), tan (0): value of the arc function tangent to the spatial angle 0. - of the fifth calculation means (M5) of a corrected tangent arc function: tan ', ( 0) = tan (0) + Corr (tan (0)) with: tancorr (0): corrected tangent arc function, tan (0): tangent arc function, Corr (tan (0)): correction on tangent arc function at the spatial angle 0. - means for determining (MD) the position (0) of the target (T) along the axis (X) from the thus corrected tangent arc function (tancorr (0) )).
    [0004]
    4. Motor vehicle characterized in that it comprises an inductive sensor (10) according to the preceding claim.
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    WO2021229169A1|2021-11-18|Method and device for measuring the mechanical angular position of a rotor
    WO2017212151A1|2017-12-14|Apparatus for measuring the angular position of a shaft or the like
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    EP3769046A1|2021-01-27|Method of measuring a position of a movable body relative to a fixed body
    FR3088717A1|2020-05-22|DETECTION SYSTEM FOR STEERING A VEHICLE FOR MEASURING TORQUE AND ABSOLUTE MULTI-TURN ANGLE
    同族专利:
    公开号 | 公开日
    FR3036790B1|2017-06-02|
    US10317249B2|2019-06-11|
    CN106197238A|2016-12-07|
    US20160349084A1|2016-12-01|
    CN106197238B|2019-11-19|
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    法律状态:
    2016-05-20| PLFP| Fee payment|Year of fee payment: 2 |
    2016-12-02| PLSC| Publication of the preliminary search report|Effective date: 20161202 |
    2017-05-23| PLFP| Fee payment|Year of fee payment: 3 |
    2018-05-22| PLFP| Fee payment|Year of fee payment: 4 |
    2019-05-23| PLFP| Fee payment|Year of fee payment: 5 |
    2020-05-22| PLFP| Fee payment|Year of fee payment: 6 |
    2021-04-16| TP| Transmission of property|Owner name: CONTINENTAL AUTOMOTIVE FRANCE, FR Effective date: 20210309 Owner name: CONTINENTAL AUTOMOTIVE GMBH, DE Effective date: 20210309 |
    2021-05-20| PLFP| Fee payment|Year of fee payment: 7 |
    2022-02-11| CA| Change of address|Effective date: 20220103 |
    优先权:
    申请号 | 申请日 | 专利标题
    FR1554773A|FR3036790B1|2015-05-27|2015-05-27|METHOD FOR DETERMINING THE POSITION OF A MOBILE PIECE ALONG AN AXIS USING AN INDUCTIVE SENSOR|FR1554773A| FR3036790B1|2015-05-27|2015-05-27|METHOD FOR DETERMINING THE POSITION OF A MOBILE PIECE ALONG AN AXIS USING AN INDUCTIVE SENSOR|
    US15/165,101| US10317249B2|2015-05-27|2016-05-26|Method for determining the position of a moving part along an axis, using an inductive sensor|
    CN201610355927.6A| CN106197238B|2015-05-27|2016-05-26|For using inductosyn to determine moving parts along the method for the position of axis|
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