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ADIS16400/PCBZ Datasheet(PDF) 15 Page - Analog Devices |
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ADIS16400/PCBZ Datasheet(HTML) 15 Page - Analog Devices |
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15 / 20 page ![]() ADIS16400/ADIS16405 Rev. B | Page 15 of 20 Auxiliary DAC The 12-bit AUX_DAC line can drive its output to within 5 mV of the ground reference when it is not sinking current. As the output approaches 0 V, the linearity begins to degrade (~100 LSB beginning point). As the sink current increases, the nonlinear range increases. The DAC latch command moves the values of the AUX_DAC register into the DAC input register, enabling both bytes to take effect at the same time. Table 20. AUX_DAC Bits Description Default = 0x0000 [15:12] Not used. [11:0] Data bits. Scale factor = 0.8059 mV/code, offset binary format, 0 V = 0 codes. Table 21. Setting AUX_DAC = 1 V DIN Description 0xB0D9 AUX_DAC[7:0] = 0xD9 (217 LSB). 0xB104 AUX_DAC[15:8] = 0x04 (1024 LSB). 0xBE04 GLOB_CMD[2] = 1. Move values into the DAC input register, resulting in a 1 V output level. DIAGNOSTICS Self-Test The self-test function offers the opportunity to verify the mechanical integrity of each MEMS sensor. It applies an electrostatic force to each sensor element, which results in mechanical displacement that simulates a response to actual motion. Table 1 lists the expected response for each sensor, which provides pass/fail criteria. Set MSC_CTRL[10] = 1 (DIN = 0xB504) to run the internal self-test routine, which exercises all inertial sensors, measures each response, makes pass/fail decisions, and reports them to error flags in the DIAG_STAT register. MSC_CTRL[10] resets itself to 0 after completing the routine. MSC_CTRL[9:8] (DIN = 0xB502 or 0xB501) provide manual control over the self-test function. Table 22 shows an example test flow for using this option to check the x-axis gyroscope. Zero motion provides results that are more reliable. The settings in Table 22 are flexible and provide opportunity for optimization around speed and noise influence. For example, using fewer filtering taps decreases delay times but increases the opportunity for noise influence. Memory Test Setting MSC_CTRL[11] = 1 (DIN = 0xB508) performs a checksum verification of the flash memory locations. The pass/fail result loads into the DIAG_STAT[6] register. Status The error flags provide indicator functions for common system- level issues. All of the flags clear (set to 0) after each DIAG_STAT register read cycle. If an error condition remains, the error flag returns to 1 during the next sample cycle. DIAG_STAT[1:0] does not require a read of this register to return to 0. Table 22. Manual Self-Test Example Sequence DIN Description 0xB601 SMPL_PRD[7:0] = 0x01, sample rate = 819.2 SPS. 0xB904 SENS_AVG[15:8] = 0x04, gyroscope range = ±300°/sec. 0xB802 SENS_AVG[7:0] = 0x02, four-tap averaging filter. Delay = 50 ms. 0x0400 Read XGYRO_OUT. 0xB502 MSC_CTRL[9] = 1, gyroscope negative self-test. Delay = 50 ms. 0x0400 Read XGYRO_OUT. Calculate the positive change from the first reading to the second reading of XGYRO_OUT, and check to make sure the change is within the positive self-test response range specified in Table 1. 0xB501 MSC_CTRL[9:8] = 01, gyroscope/accelerometer positive self-test. Delay = 50 ms. 0x0400 Read XGYRO_OUT. Calculate the negative change from the first reading to the third reading of XGYRO_OUT, and check to make sure the change is within the positive self-test response range specified in Table 1 . 0xB500 MSC_CTRL[15:8] = 0x00. Table 23. DIAG_STAT Bit Descriptions Bit Description [15] Z-axis accelerometer self-test failure (1 = fail, 0 = pass) [14] Y-axis accelerometer self-test failure (1 = fail, 0 = pass) [13] X-axis accelerometer self-test failure (1 = fail, 0 = pass) [12] Z-axis gyroscope self-test failure (1 = fail, 0 = pass) [11] Y-axis gyroscope self-test failure (1 = fail, 0 = pass) [10] X-axis gyroscope self-test failure (1 = fail, 0 = pass) [9] Alarm 2 status (1 = active, 0 = inactive) [8] Alarm 1 status (1 = active, 0 = inactive) [7] Not used [6] Flash test, checksum flag (1 = fail, 0 = pass) [5] Self-test diagnostic error flag (1 = fail, 0 = pass) [4] Sensor overrange (1 = fail, 0 = pass) [3] SPI communication failure (1 = fail, 0 = pass) [2] Flash update failure (1 = fail, 0 = pass) [1] Power supply above 5.25 V (1 = power supply ≥ 5.25 V, 0 = power supply ≤ 5.25 V) [0] Power supply below 4.75 V (1 = power supply ≤ 4.75 V, 0 = power supply ≥ 4.75 V) |
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