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ADIS16204 Просмотр технического описания (PDF) - Analog Devices

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ADIS16204 Datasheet PDF : 24 Pages
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ADIS16204
THEORY OF OPERATION
OVERVIEW
IMPACT/SHOCK RESPONSE
The ADIS16204 integrates a dual-axis ±70 g/±37 g MEMS
The sensor’s mechanical structure provides a linear meas-
acceleration sensor into a complete impact/shock measurement
urement range that is 8 times that of each axis’ actual output
and recording system. The integrated mixed signal processing
measurement range. Therefore, when considering the response
circuit digitizes the sensor data, applies corrections factors,
to high-g, short duration events, the 2-pole, 400 Hz, low-pass
provides many user-programmable features, and offers a simple
Bessel filter network influences the output response. Figure 18
communication conduit: the serial peripheral interface (SPI).
provides a frequency response for this signal chain. In Figure 19,
ACCELERATION SENSOR
the X-axis accelerometer experiences a 560 g shock event that
lasts 0.1 ms, causing the output response to reach 70 g. For users
The ADIS16204 base sensor core provides a fully differential
sensor structure and circuit path, resulting in substantial
rejection of electromagnetic interference (EMI) effects. It
uses electrical feedback with zero-force feedback for improved
accuracy and stability. The sensor’s resonant frequency is well
E beyond the cut-off frequency of the filter, which adds further
noise rejection to the sensor signal conditioning circuit.
ANCHOR
T PLATE
CAPACITORS
UNIT
E SENSING
CELL
FIXED
PLATES
MOVABLE
FRAME
L MOVING
PLATE
UNIT
FORCING
CELL
ANCHOR
O Figure 17. Simplified View of a Sensor Under Acceleration
Figure 17 is a simplified view of one of the differential sensor
S elements. Each sensor includes several differential capacitor
unit cells. Each cell is composed of fixed plates attached to the
substrate and movable plates attached to the frame. Displace-
ment of the frame changes the differential capacitance, which
B is measured by the on-chip circuitry.
Complementary 200 kHz square waves drive the fixed plates.
Electrical feedback adjusts the amplitudes of the square waves
O such that the ac signal on the moving plates is 0 V. The feedback
that need to avoid output saturation, keeping the integration of
the event’s acceleration response (acceleration-time product in
the case of Figure 19) below 56 g-ms is critical.
10
X: 418.9
0
Y: –3.291
–10
–20
–30
–40
–50
10
100
1k
10k
FREQUENCY (Hz)
Figure 18. ADIS16204 Frequency Response
600
550
560g, 0.1ms, SIMULATED SHOCK
500
450
400
350
300
250
200
150
70g, FILTERED RESPONSE
100
50
signal is linearly proportional to the applied acceleration. This
0
–0.50 –0.25 0 0.25 0.50 0.75 1.00 1.25 1.50 1.75 2.00
unique feedback technique ensures that there is no net electro-
TIME (ms)
static force applied to the sensor. The differential feedback control
Figure 19. ADIS16204 Shock Response
signal is also applied to the input of the filter, where it is filtered
and converted to a single-ended signal.
TEMPERATURE SENSOR
This sensor reflects the sensor’s junction temperature and
provides a convenient temperature measurement for system-
level characterization and calibration feedback.
Rev. B | Page 10 of 24

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