MMA1260EGR2

MMA1260KEG
Sensors
4 Freescale Semiconductor
PRINCIPLE OF OPERATION
The Freescale 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 integrated 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 semiconductor
processes (masking and etching). It can be modeled as two
stationary plates with a moveable plate in-between. The
center plate can be deflected from its rest position by
subjecting the system to an acceleration (Figure 3).
When the center plate deflects, the distance from it to one
fixed plate will increase by the same amount that the distance
to the other plate decreases. The change in distance is a
measure of acceleration.
The g-cell plates form two back-to-back capacitors
(Figure 4). As the center plate moves with acceleration, the
distance between the plates changes and each capacitor's
value will change, (C = Aε/D). Where A is the area of the
plate, ε is the dielectric constant, and D is the distance
between the plates.
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
ratiometric and proportional to acceleration.
SPECIAL FEATURES
Filtering
The Freescale accelerometers contain an onboard 2-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
filter 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
verification of the mechanical and electrical integrity of the
accelerometer 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 electrostatic
force (Fe =
1
/
2
AV
2
/d
2
) causes the center plate to deflect. The
resultant deflection is measured by the accelerometer's
control ASIC and a proportional output voltage results. This
procedure assures that both the mechanical (g-cell) and
electronic sections of the accelerometer are functioning.
Status
Freescale 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 the
following event occurs:
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.
Acceleration
Figure 3. Transducer
Physical Model
Figure 4. Equivalent
Circuit Model
MMA1260KEG
Sensors
Freescale Semiconductor 5
BASIC CONNECTIONS
Pinout Description
Figure 5. SOIC Accelerometer with Recommended
Connection Diagram
PCB Layout
Figure 6. Recommended PCB Layout for Interfacing
Accelerometer to Microcontroller
NOTES:
1. Use a 0.1 μF capacitor on V
DD
to decouple the power
source.
2. Physical coupling distance of the accelerometer to the
microcontroller should be minimal.
3. Place a ground plane beneath the accelerometer to
reduce noise, the ground plane should be attached to
all of the open ended terminals shown in Figure 6.
4. Use an RC filter of 1 kΩ and 0.1 μF on the output of the
accelerometer to minimize clock noise (from the
switched capacitor filter circuit).
5. PCB layout of power and ground should not couple
power supply noise.
6. Accelerometer and microcontroller should not be a
high current path.
7. A/D sampling rate and any external power supply
switching frequency should be selected such that they
do not interfere with the internal accelerometer
sampling frequency. This will prevent aliasing errors.
Table 3. Pin Descriptions
Pin No. Pin Name Description
1 thru 3 V
SS
Redundant connections to the internal
V
SS
and may be left unconnected.
4 V
OUT
Output voltage of the accelerometer.
5 STATUS Logic output pin to indicate fault.
6 V
DD
The power supply input.
7 V
SS
The power supply ground.
8 ST Logic input pin used to initiate self-test.
9 thru 13 Trim pins Used for factory trim. Leave
unconnected.
14 thru 16 No internal connection. Leave
unconnected.
V
SS
V
SS
V
SS
V
OUT
STATUS
V
DD
V
SS
ST
N/C
N/C
N/C
N/C
N/C
N/C
N/C
N/C
1
2
3
4
5
6
7
8
16
15
14
13
12
11
10
9
8
MMA1260KEG
ST
V
DD
V
SS
V
OUT
Output
Signal
R1
1 kΩ
4
C2
0.1 μF
6
7
Logic
Input
V
DD
C1
0.1 μF
STATUS
5
3
2
1
V
SS
V
SS
V
SS
P0
A/D In
V
RH
V
SS
V
DD
ST
V
OUT
V
SS
V
DD
0.1 μF1 kΩ
0.1 μF
0.1 μF
Power Supply
0.1 μF
P1STATUS
Microcontroller
Accelerometer
C
C
C
R
C
MMA1260KEG
Sensors
6 Freescale Semiconductor
1. When positioned as shown, the Earth's gravity will result in a positive 1g output
ACCELERATION SENSING DIRECTIONS
10
11
12
13
14
15
16
8
7
6
5
4
3
2
1
9
V
SS
V
SS
V
SS
V
OUT
STATUS
V
DD
V
SS
N/C
N/C
N/C
N/C
N/C
N/C
N/C
N/C
16-Pin SOIC Package
N/C pins are recommended to be left FLOATING
–g
+g
Direction of Earth's gravity field
(1)
DYNAMIC ACCELERATION
STATIC ACCELERATION
-1g
+1g
0g 0g
V
OUT
= 2.50 V V
OUT
= 2.50 V
V
OUT
= 3.7 V
V
OUT
= 1.3 V
ST

MMA1260EGR2

Mfr. #:
Manufacturer:
NXP / Freescale
Description:
Accelerometers COLOSUS 1.5
Lifecycle:
New from this manufacturer.
Delivery:
DHL FedEx Ups TNT EMS
Payment:
T/T Paypal Visa MoneyGram Western Union

Products related to this Datasheet