Systems, methods and apparatuses for guidance and alignment in electric vehicles wireless inductive charging systems
US-2016380488-A1 · Dec 29, 2016 · US
US2016349084A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016349084-A1 |
| Application number | US-201615165101-A |
| Country | US |
| Kind code | A1 |
| Filing date | May 26, 2016 |
| Priority date | May 27, 2015 |
| Publication date | Dec 1, 2016 |
| Grant date | — |
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A method for determining the position θ of a moving part (T) along an axis (X), using an inductive sensor ( 10 ) including: a primary winding (B 1 ) generating an electromagnetic field; a first secondary winding (R 1 ), generating a first voltage signal (V 1 ), of the sine function type; a second secondary winding (R 2 ), generating a second voltage signal (V 2 ) of the cosine function type; and a calculation unit ( 20 ′), wherein the method includes the steps of calculating and distributing linearization points i on the arctangent function tan(θ) resulting from the ratio of the first voltage signal to 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 (E 1 , E 2 ) of the primary and secondary windings (R 1 , R 2 ).
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1 . 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 (B 1 ) generating an electromagnetic field, a first secondary winding (R 1 ), generating a first voltage signal (V 1 ) of the sine function type, representing the current induced in said first secondary winding (R 1 ) when the target (T) moves in front of the first secondary winding (R 1 ), a second secondary winding (R 2 ), generating a second voltage signal (V 2 ) of the cosine function type, representing the current induced in said second secondary winding (R 2 ) when the target moves in front of the second secondary winding (R 2 ), a calculation unit ( 20 ′), said determination method including the following steps: Step 1: calculating an arctangent function (tan(θe)) on the basis of the first voltage signal (V 1 ) and the second voltage signal (V 2 ), Step 2: calculating an error (ε(θ)) between the arctangent function (tan(θ)) calculated in this way and a predetermined straight line (D L ), Step 3: calculating the positions of linearization points (θ i ) of the arctangent function (tan(θ)) according to the formula θ i = ( i - 1 ) × C u ( n - 1 ) - [ sin ( ( i - 1 ) × 2 × π ( n - 1 ) ) × F × C u ] where: i is the index of the linearization points, varying from 1 to n, θ i is the position of the linearization point i as a spatial angle, F is the spacing factor of the linearization points, where F>0 and F MAX is such that: F MAX < ( i - 1 ) × C u ( n - 1 ) - [ sin ( ( i - 1 ) × 2 × π ( n - 1 ) ) × C u ] C u is the useful travel of the sensor along the axis as a spatial angle. Step 4: for each value of the arctangent function (tan(θ)), finding an index (i) of the linearization point such that: θ i <θ<θ i+1 where: θ i is the position of the linearization point i as a spatial angle, θ i+1 is the position of the linearization point (i+1) as a spatial angle, θ is a spatial angle. Step 5: calculating a correction to be applied to the arctangent function (tan(θ)) according to the formula Corr ( tan ( θ ) ) = ɛ ( θ i ) + [ ɛ ( θ i + 1 ) - ɛ ( θ i )
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