4Motorola Sensor Device Data
MMA3202D
PRINCIPLE OF OPERATION
The Motorola accelerometer is a surface--micromachined
integrated--circuit accelerometer. The device consists of a
surface micromachined capacitive sensing cell (g--cell) and a
CMOS signal conditioning ASIC contained in a single inte-
grated circuit package. The sensing element is sealed
hermetically at the wafer level using a bulk micromachined
”cap’’ wafer. The g--cell is a mechanical structure formed
from semiconductor materials (polysilicon) using semicon-
ductor processes (masking and etching). It can be modeled
as a set of beams attached to a movable central mass that
move between fixed beams. The movable beams can be de-
flected from their rest position by subjecting the system to an
acceleration. As the beams attached to the central mass
move the distance from them to the fixed beams on one side
will increase by the same amount that the distance to the
fixed beams on the other side decreases.
The change in distance is a measure of acceleration. The
g--cell beams form two back--to--back capacitors (Figure 2).
As the central mass moves with acceleration, the distance
between the beams change and each capacitor’s value will
change, (C = NAe/D). Where A is the area of the facing side
of the beam, e is the dielectric constant, and D is the distance
between the beams and N is the number of beams.
The CMOS ASIC uses switched capacitor techniques to
measure the g--cell capacitors and extract the acceleration
data from the difference between the two capacitors. The
ASIC also signal conditions and filters (switched capacitor)
the signal, providing a high level output voltage that is ratio-
metric and proportional to acceleration.
Acceleration
Figure 2. Simplified Transducer Physical Model
versus Transducer Physical Model
SPECIAL FEATURES
Filtering
The Motorola accelerometers contain an onboard 4--pole
switched capacitor filter. A Bessel implementation is used
because it provides a maximally flat delay response (linear
phase) thus preserving pulse shape integrity. Because the fil-
ter is realized using switched capacitor techniques, there is
no requirement for external passive components (resistors
and capacitors) to set the cut--off frequency.
Self--Test
The sensor provides a self--test feature that allows the ver-
ification of the mechanical and electrical integrity of the ac-
celerometer at any time before or after installation. This
feature is critical in applications such as automotive airbag
systems where system integrity must be ensured over the life
of the vehicle. A fourth “plate’’ is used in the g--cell as a self--
test plate. When the user applies a logic high input to the
self--test pin, a calibrated potential is applied across the
self--test plate and the moveable plate. The resulting elec-
trostatic force (Fe = 1/2AV2/d2) causes the center plate to
deflect. The resultant deflection is measured by the accel-
erometer’s control ASIC and a proportional output voltage re-
sults. This procedure assures that both the mechanical
(g--cell) and electronic sections of the accelerometer are
functioning.
Ratiometricity
Ratiometricity simply means that the output offset voltage
and sensitivity will scale linearly with applied supply voltage.
That is, as you increase supply voltage the sensitivity and
offset increase linearly; as supply voltage decreases, offset
and sensitivity decrease linearly. This is a key feature when
interfacing to a microcontroller or an A/D converter because
it provides system level cancellation of supply induced errors
in the analog to digital conversion process.
Status
Motorola accelerometers include fault detection circuitry
and a fault latch. The Status pin is an output from the fault
latch, OR’d with self--test, and is set high whenever one (or
more) of the following events occur:
•Supply voltage falls below the Low Voltage Detect (LVD)
voltage threshold
•Clock oscillator falls below the clock monitor minimum
frequency
•Parity of the EPROM bits becomes odd in number.
The fault latch can be reset by a rising edge on the self--
test input pin, unless one (or more) of the fault conditions
continues to exist.
BASIC CONNECTIONS
Pinout Description
14
15
16
17
18
19
20
8
7
6
5
4
3
2
1
13
N/C
N/C
N/C
ST
XOUT
STATUS
VDD
GND
N/C
N/C
N/C
N/C
N/C
N/C
N/C
12
10
9
11
VSS
AVDD
N/C
YOUT
N/C