| Electronic Components Datasheet Search |
|
ADIS16501/PCBZ Datasheet(PDF) 14 Page - Analog Devices |
|
|
|||||||||||||||||||||||||||||
ADIS16501/PCBZ Datasheet(HTML) 14 Page - Analog Devices |
|
14 / 45 page ![]() Data Sheet ADIS16501 TERMINOLOGY analog.com Rev. B | 14 of 45 Output Full-Scale Range Output full-scale range is the guaranteed angular rate and acceler- ation measurement range at the output of the signal chain. The output full-scale range is specified as a minimum value and is guaranteed across all conditions. Angular rate and acceleration measurement are possible beyond this value. However, perform- ance characteristics are not guaranteed. Bias Bias is any static (DC) error term on the output of the ADIS16501. It is measured as the deviation from 0°/sec or 0 g without externally applied angular rate or acceleration (including gravity). Bias is measured after the device is soldered to the application PCB. To reduce the influence of external physical stimuli that may exist in the measurement system, average bias over a sufficiently long time window. Additionally, a data rate of >1 kHz is recommended. Gyroscope = ΩMEAS (ΩIN = 0°/sec) To calculate accelerometer bias, take measurements at orientations of +1 g and −1 g and calculate the average value of the two measurements. XL=ACCMEASgIN=+1g+ACCMEASgIN=−1g 2 Figure 21. Acceleration Sensitivity Measurement Process Bias Error over Temperature Bias error over temperature is the change in bias directly attrib- uted to changes in temperature. Bias error over temperature is measured relative to the bias at 25°C. Figure 22 shows the bias error over temperature expected for a device with a bias at 25°C equivalent to the initial (start of life) bias. Bias drift over life can cause the offset measured at 25°C to diverge from the initial (start of life) bias measured during module manufacture. Figure 23 shows how the bias error over temperature limits is adjusted to accommodate the divergence of the bias at 25°C and the initial bias. Figure 22. Bias Error over Temperature, OFFINIT = OFFAT_25°C Figure 23. Bias Error over Temperature, OFFINIT ≠ OFFAT_25°C (Change OF- FAT_25°C to OFFAT_25°C) Bias Repeatability Bias repeatability describes the long-term offset behavior over a variety of conditions. Bias repeatability represents a projection for long-term aging, which is derived from the drift behaviors that a sample of units exhibits throughout a 1000-hour, 110°C high temperature operating life (HTOL) stress. In-Run Bias Stability In-run bias (offset) stability is a measure of how quickly gyroscope (or accelerometer) outputs drift over time. In-run bias stability is derived from the minimum of the Allan variance curve as follows: Accelerometer Allan Variance(τ) = 12n−1 ∑iACCMEASτi+1−ACCMEASτi2 Gyroscope Allan Variance(τ) = 12n−1 ∑iΩMEASτi+1−ΩMEASτi2 |
|
Link URL |
| Does ALLDATASHEET help your business so far? [ DONATE ] |
About Alldatasheet | Advertisement | Contact us | Privacy Policy | Link to Datasheet | Link Exchange | Manufacturer List All Rights Reserved©Alldatasheet.com |
| Russian : Alldatasheetru.com | Korean : Alldatasheet.co.kr | Spanish : Alldatasheet.es | French : Alldatasheet.fr | Italian : Alldatasheetit.com Portuguese : Alldatasheetpt.com | Polish : Alldatasheet.pl | Vietnamese : Alldatasheet.vn Indian : Alldatasheet.in | Mexican : Alldatasheet.com.mx | British : Alldatasheet.co.uk | New Zealand : Alldatasheet.co.nz |
|
Family Site : ic2ic.com |
icmetro.com |