MOTOROLA MA126

Freescale Semiconductor
Technical Data
MMA1260D
Rev. 1, 10/2004
Low G
Micromachined Accelerometer
MMA1260D
The MMA series of silicon capacitive, micromachined accelerometers
features signal conditioning, a 2--pole low pass filter and temperature
compensation. Zero--g offset full scale span and filter cut--off are factory set and
require no external devices. A full system self--test capability verifies system
functionality.
MMA1260D: Z AXIS SENSITIVITY
MICROMACHINED
ACCELEROMETER
±1.5g
Features
• Integral Signal Conditioning
• Linear Output
• 2nd Order Bessel Filter
• Calibrated Self--test
• EPROM Parity Check Status
16
• Transducer Hermetically Sealed at Wafer Level for Superior Reliability
• Robust Design, High Shock Survivability
9
1
Typical Applications
8
• Vibration Monitoring and Recording
16 LEAD SOIC
CASE 475--01
• Appliance Control
• Mechanical Bearing Monitoring
• Computer Hard Drive Protection
• Computer Mouse and Joysticks
Pin Assignment
• Virtual Reality Input Devices
• Sports Diagnostic Devices and Systems
VSS
VSS
VSS
VOUT
ORDERING INFORMATION
Device
Temperature Range
MMA1260D
--40 to +105°C
Case No.
Package
Case 475--01
SOIC--16
STATUS
VDD
VSS
ST
16
15
14
13
12
11
10
1
2
3
4
5
6
7
8
9
N/C
N/C
N/C
N/C
N/C
N/C
N/C
N/C
SIMPLIFIED ACCELEROMETER FUNCTIONAL BLOCK DIAGRAM
VDD
G--CELL
SENSOR
ST
SELF--TEST
INTEGRATOR
GAIN
CONTROL LOGIC &
EPROM TRIM CIRCUITS
FILTER
OSCILLATOR
TEMP COMP
& GAIN
CLOCK GEN.
VOUT
VSS
STATUS
Figure 1. Simplified Accelerometer Functional Block Diagram
REV 1
© Freescale Semiconductor, Inc., 2004. All rights reserved.
Sensor Device Data
Freescale Semiconductor
MMA1260D
1
MAXIMUM RATINGS (Maximum ratings are the limits to which the device can be exposed without causing permanent damage.)
Symbol
Value
Unit
Powered Acceleration (all axes)
gpd
1500
g
Unpowered Acceleration (all axes)
gupd
2000
g
Supply Voltage
VDD
--0.3 to +7.0
V
Hdrop
1.2
m
Tstg
--40 to +125
°C
Rating
Drop
Test(1)
Storage Temperature Range
NOTES:
1. Dropped onto concrete surface from any axis.
ELECTRO STATIC DISCHARGE (ESD)
WARNING: This device is sensitive to electrostatic
discharge.
Although the Freescale Semiconductor accelerometers
contain internal 2kV ESD protection circuitry, extra precaution must be taken by the user to protect the chip from ESD.
A charge of over 2000 volts can accumulate on the human
body or associated test equipment. A charge of this magnitude can alter the performance or cause failure of the chip.
When handling the accelerometer, proper ESD precautions
should be followed to avoid exposing the device to discharges which may be detrimental to its performance.
MMA1260D
2
Sensor Device Data
Freescale Semiconductor
OPERATING CHARACTERISTICS
(Unless otherwise noted: --40°C ≤ TA ≤ +105°C, 4.75 ≤ VDD ≤ 5.25, Acceleration = 0g, Loaded output(1))
Symbol
Min
Typ
Max
Unit
VDD
IDD
TA
gFS
4.75
1.1
−40
—
5.00
2.2
—
1.5
5.25
3.2
+105
—
V
mA
°C
g
VOFF
VOFF
S
S
f --3dB
NLOUT
2.25
2.2
1140
1110
40
−1.0
2.5
2.5
1200
1200
50
—
2.75
2.8
1260
1290
60
+1.0
V
V
mV/g
mV/g
Hz
% FSO
Noise
RMS (0.1 Hz -- 1.0 kHz)
Spectral Density (RMS, 0.1 Hz -- 1.0 kHz)(6)
nRMS
nSD
—
—
5.0
500
9.0
—
mVrms
µg/√Hz
Self--Test
Output Response (VDD = 5.0 V)
Input Low
Input High
Input Loading(7)
Response Time(8)
∆VST
VIL
VIH
IIN
tST
0.3
VSS
0.7 VDD
−50
—
0.6
—
—
−125
10
0.9
0.3 VDD
VDD
−300
25
V
V
V
µA
ms
Status(12)(13)
Output Low (Iload = 100 µA)
Output High (Iload = --100 µA)
VOL
VOH
—
VDD −0.8
—
—
0.4
—
V
V
Output Stage Performance
Electrical Saturation Recovery Time(9)
Full Scale Output Range (IOUT = --200 µA)
Capacitive Load Drive(10)
Output Impedance
tDELAY
VFSO
CL
ZO
—
VSS+0.25
—
—
—
—
—
50
2.0
VDD−0.25
100
—
ms
V
pF
Ω
Mechanical Characteristics
Transverse Sensitivity(11)
VXZ,YZ
—
—
5.0
% FSO
Characteristic
Range(2)
Operating
Supply Voltage(3)
Supply Current
Operating Temperature Range
Acceleration Range
Output Signal
Zero g (TA = 25°C, VDD = 5.0 V)(4)
Zero g (VDD = 5.0 V)
Sensitivity (TA = 25°C, VDD = 5.0 V)(5)
Sensitivity (VDD = 5.0 V)
Bandwidth Response
Nonlinearity
NOTES:
1. For a loaded output the measurements are observed after an RC filter consisting of a 1 kΩ resistor and a 0.1 µF capacitor to ground.
2. These limits define the range of operation for which the part will meet specification.
3. Within the supply range of 4.75 and 5.25 volts, the device operates as a fully calibrated linear accelerometer. Beyond these supply limits
the device may operate as a linear device but is not guaranteed to be in calibration.
4. The device can measure both + and − acceleration. With no input acceleration the output is at midsupply. For positive acceleration the output
will increase above VDD/2 and for negative acceleration the output will decrease below VDD/2.
5. Sensitivity limits apply to 0 Hz acceleration.
6. At clock frequency ≅ 34 kHz.
7. The digital input pin has an internal pull--down current source to prevent inadvertent self test initiation due to external board level leakages.
8. Time for the output to reach 90% of its final value after a self--test is initiated.
9. Time for amplifiers to recover after an acceleration signal causing them to saturate.
10. Preserves phase margin (60°) to guarantee output amplifier stability.
11. A measure of the device’s ability to reject an acceleration applied 90° from the true axis of sensitivity.
12. The Status pin output is not valid following power--up until at least one rising edge has been applied to the self--test pin. The Status pin is
high whenever the self--test input is high.
13. The Status pin output latches high if the EPROM parity changes to odd. The Status pin can be reset by a rising edge on self--test, unless
a fault condition continues to exist.
MMA1260D
Sensor Device Data
Freescale Semiconductor
3
PRINCIPLE OF OPERATION
SPECIAL FEATURES
The Freescale Semiconductor 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 2).
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 3). 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.
Filtering
The Freescale Semiconductor 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.
Acceleration
Figure 2. Transducer
Physical Model
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. 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 AV2/d2) 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 Semiconductor 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.
Figure 3. Equivalent
Circuit Model
MMA1260D
4
Sensor Device Data
Freescale Semiconductor
BASIC CONNECTIONS
9
ACCELEROMETER
STATUS
VDD
VSS
ST
STATUS
N/C
N/C
N/C
N/C
N/C
N/C
N/C
N/C
16
15
14
13
12
11
10
1
2
3
4
5
6
7
8
P1
ST
P0
VOUT
R
VSS
1 kΩ
VDD
A/D IN
C 0.1 µF
C 0.1 µF
VRH
C
MICROCONTROLLER
VSS
VSS
VSS
VOUT
PCB Layout
VSS
C 0.1 µF
VDD
0.1 µF
Figure 4. Pinout Description
POWER SUPPLY
Pin No.
Pin Name
Description
1 thru 3
VSS
Redundant connections to the internal
VSS and may be left unconnected.
4
VOUT
5
STATUS
6
VDD
The power supply input.
7
VSS
The power supply ground.
NOTES:
8
ST
Logic input pin used to initiate self-test.
9 thru 13
Trim pins
Used for factory trim.
Leave unconnected.
• Use a 0.1 µF capacitor on VDD to decouple the power
source.
14 thru 16
—
No internal connection.
Leave unconnected.
VDD
Output voltage of the accelerometer.
Logic output pin used to indicate fault.
MMA1260D
LOGIC
INPUT
Figure 6. Recommended PCB Layout for Interfacing
Accelerometer to Microcontroller
5
8 ST
6 VDD
C1
0.1 µF
7 VSS
VOUT 4
• Physical coupling distance of the accelerometer to the microcontroller should be minimal.
• Place a ground plane beneath the accelerometer to reduce
noise, the ground plane should be attached to all internal
VSS terminals shown in Figure 4.
STATUS
R1
1 kΩ
OUTPUT
SIGNAL
C2
0.1 µF
Figure 5. SOIC Accelerometer with Recommended
Connection Diagram
• 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).
• PCB layout of power and ground should not couple power
supply noise.
• Accelerometer and microcontroller should not be a high
current path.
• 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.
MMA1260D
Sensor Device Data
Freescale Semiconductor
5
ACCELERATION SENSING DIRECTIONS
DYNAMIC ACCELERATION
VSS
VSS
VSS
VOUT
+g
STATUS
VDD
VSS
ST
1
2
3
4
5
6
7
8
16
15
14
13
12
11
10
9
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
STATIC ACCELERATION
Direction of Earth’s gravity field.*
+1g
VOUT = 3.7V
0g
0g
VOUT = 2.50V
VOUT = 2.50V
--1g
VOUT = 1.3V
* When positioned as shown, the Earth’s gravity will result in a positive 1g output
MMA1260D
6
Sensor Device Data
Freescale Semiconductor
PACKAGE DIMENSIONS
A
A
G/2
2 PLACES, 16 TIPS
G
16
NOTES:
1. ALL DIMENSIONS ARE IN MILLIMETERS.
2. INTERPRET DIMENSIONS AND TOLERANCES
PER ASME Y14.5M, 1994.
3. DIMENSIONS ”A” AND ”B” DO NOT INCLUDE
MOLD FLASH OR PROTRUSIONS. MOLD FLASH
OR PROTRUSIONS SHALL NOT EXCEED 0.15
PER SIDE.
4. DIMENSION ”D” DOES NOT INCLUDE DAMBAR
PROTRUSION. PROTRUSIONS SHALL NOT
CAUSE THE LEAD WIDTH TO EXCEED 0.75
0.15 T A B
9
B
P
1
B
8
16X
D
0.13
M
T A B
R
J
C
0.1
T
X 45 _
K
F
DIM
A
B
C
D
F
G
J
K
M
P
R
MILLIMETERS
MIN
MAX
10.15
10.45
7.40
7.60
3.30
3.55
0.35
0.49
0.76
1.14
1.27 BSC
0.25
0.32
0.10
0.25
0_
7_
10.16
10.67
0.25
0.75
M
SEATING
PLANE
CASE 475--01
ISSUE B
16 LEAD SOIC
MMA1260D
Sensor Device Data
Freescale Semiconductor
7
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© Freescale Semiconductor, Inc. 2004. All rights reserved.
MMA1260D
Rev. 1
10/2004
MMA1260D
8
Sensor Device Data
Freescale Semiconductor