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L9374LF датащи(PDF) 34 Page - STMicroelectronics |
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L9374LF датащи(HTML) 34 Page - STMicroelectronics |
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34 / 80 page ![]() Circuit description L9374LF 34/80 DocID025414 Rev 1 SWT values) the parameters Set-Point 1 (DUTY1 or CUR/DTY1), Set-Point 2 (DUTY2 or CUR/DTY2) and duration t1 (D_Qx) are programmed (for programming instructions see section 5.1.5: Duration registers (address 4 and 5)). Generically, after the SYNC_TRIG the Set-Point 1 is valid for t1 ms. After t1 ms the set-point controller switches to Set-Point 2 until the next SYNC_TRIG event. Figure 20. Set-point control example In this example the RESET_VALUE (and therefore the SPI transfer loop time) is set to 5ms and the SYNC_VALUE is set to 2.5 ms. This sets the SYNC_TRIG at 2.5 ms after each SPI transfer. At SYNC_TRIG, the new information received at the previous SPI transfer is incorporated into the Set-Point Controller. 4.5 Current controller Two outputs (Q3 & Q4) are equipped with a current controller. The current controller converts the Set-Point controller output (Current Set Point) into a current level regulated duty cycle command using a sophisticated algorithm incorporating Load resistance supply voltage, and recirculation path variances. The current controller output duty cycle information is calculated using a dedicated load model in standard Arithmetic Logic Unit (ALU). This model includes the supply voltage, the recirculation path as well as the load resistance. The load resistance value is programmable via SPI while the recirculation path and the load supply voltage parameters are measured by the L9374LF. These measured values are readable via SPI as well. 4.5.1 Load resistance error integration phase The value of the programmed Load is corrected during the valve actuation. This correction is called the Error Integration Phase and the resulting value (ISAT_Qx,) is accessible via SPI (Status registers 8 and 9, Section 5.2.5). ISAT_Qx is an internal value of the current controller. In an ideal system (without any system tolerances) the first approximation is determined y the equation: ISAT RL_real RL_SPI --------------------- 1 – |
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