Ultra Low Noise, Low offset Drift ±1 g Dual
Axis Accelerometer with Digital Outputs
MXD2020E/F
FEATURES
Resolution better than 1 mg at 1 Hz
Dual axis accelerometer fabricated on a monolithic CMOS IC
RoHS compliant
On-chip mixed mode signal processing
50,000 g shock survival rating
17 Hz bandwidth
3.00V to 5.25V single supply operation
Small (5mm x 5mm x 2mm) surface mount package
Continuous self-test
Independent axis programmability (special order)
Sck
(optional)
Internal
Oscillator
CLK
TOUT
Voltage
Reference
VREF
Continous
Self Test
Heater
Control
X axis
Low Pass
Filter
DOUTX
Low Pass
Filter
DOUTY
Factory Adjust
Offset & Gain
APPLICATIONS
Y axis
Automotive – Vehicle Security/Active Suspension/ABS
Headlight Angle Control/Tilt Sensing
Security – Gas Line/Elevator/Fatigue Sensing
Office Equipment – Computer Peripherals/PDA’s/Cell Phones
Gaming – Joystick/RF Interface/Menu Selection/Tilt Sensing
Projectors - Leveling and Keystoning
White Goods – Spin/Vibration Control
Temperature
Sensor
2-AXIS
SENSOR
VDD
Gnd
VDA
MXD2020E/F FUNCTIONAL BLOCK DIAGRAM
GENERAL DESCRIPTION
The MXD2020E/F is an ultra low noise and low cost, dual
axis accelerometer built on a standard, submicron CMOS
process. The MXD2020E/F measures acceleration with a
full-scale range of ± 1 g and a sensitivity of 20%/g @5V at
25°C. It can measure both dynamic acceleration (e.g.,
vibration) and static acceleration (e.g., gravity). The
MXD2020E/F design is based on heat convection and
requires no solid proof mass. This eliminates stiction and
particle problems associated with competitive devices and
provides shock survival up to 50,000 g, leading to
significantly lower failure rates and lower losses due to
handling during assembly.
The typical noise floor is 0.2mg / Hz allowing signals
below 1mg to be resolved at 1 Hz bandwidth. The
MXD2020E/F is available in a LCC surface mount package
(5mm x 5mm x 2mm height). It is hermetically sealed and
operational over a -40°C to +105°C temperature range.
Due to the standard CMOS structure of the MXD2020E/F,
additional circuitry can easily be incorporated into custom
versions for high volume applications. Contact the factory
for more information.
The MXD2020E/F provides two digital outputs. The
outputs are digital signals with duty cycles (ratio of pulse
width to period) that are proportional to acceleration. The
duty cycles outputs can be directly interfaced to a microprocessor.
Information furnished by MEMSIC is believed to be accurate and reliable.
However, no responsibility is assumed by MEMSIC for its use, nor for any
infringements of patents or other rights of third parties, which may result from
its use. No license is granted by implication or otherwise under any patent or
patent rights of MEMSIC
MEMSIC MXD2020E/F Rev H
Page 1 of 8
©MEMSIC, Inc.
One Technology Drive Suite 325,Andover MA01810,USA
Tel: +1 978 738 0900
Fax: + 978 738 0196
www.memsic.com
2/26/2007
MXD2020E/F SPECIFICATIONS (Measurements @ 25°C, Acceleration = 0g unless otherwise noted, VDD, VDA =
5.0V unless otherwise specified)
Parameter
SENSOR INPUT
Measurement Range1
Nonlinearity
Alignment Error2
Transverse Sensitivity3
SENSITIVITY
DOUTX and DOUTY
Change over Temperature (uncompensated)4
Change over Temperature (compensated) 4
ZERO g BIAS LEVEL
0 g Offset5
0 g Duty Cycle5
0 g Offset over Temperature
PWM output Frequency
NOISE PERFORMANCE
Noise Density, rms
FREQUENCY RESPONSE
3dB Bandwidth
TEMPERATURE OUTPUT
Tout Voltage
Sensitivity
VOLTAGE REFERENCE OUTPUT
VRef output
Change over Temperature
Current Drive Capability
SELF TEST
Continuous Voltage at DOUTX, DOUTY under
Failure
Continuous Voltage at DOUTX, DOUTY under
Failure
DOUTX and DOUTY OUTPUTS
Normal Output Range
Current
Rise/Fall Time
Turn-on Time
POWER SUPPLY
Operating Voltage Range
Supply Current
Supply Current
TEMPERATURE RANGE
Operating Range
NOTES
Conditions
Each Axis
MXD2020E/F
Typ
Max
±1.0
Best fit straight line
Each Axis
@5.0V supply
19.0
Δ from 25°C, at –40°C
Δ from 25°C, at +105°C
Δ from 25°C, –40°C to +105°C
Each Axis
Δ from 25°C
Δbased on 20%/g
For MXD2020EL only
MXD2020E
MXD2020F
@3.0V-5.25V supply
0.5
±1.0
±2.0
1.0
20.0
21.0
+120
-55
100μA typical.
While the sensitivity of this axis has been programmed at
the factory to be the same as the sensitivity for the y-axis,
the accelerometer can be programmed for non-equal
sensitivities on the x- and y-axes. Contact the factory for
additional information.
Si x Ti2.90 = Sf x Tf2.90
where Si is the sensitivity at any initial temperature Ti, and
Sf is the sensitivity at any other final temperature Tf with
the temperature values in K.
2.5
2.0
1.5
1.0
0.5
0.0
-40
-20
0
20
40
60
80
100
Temperature (C)
Figure 1: Thermal Accelerometer Sensitivity
DOUTY – This pin is the digital output of the y-axis
acceleration sensor. It is factory programmable to 100 Hz
or 400 Hz. The user should ensure the load impedance is
sufficiently high as to not source/sink >100μA typical.
While the sensitivity of this axis has been programmed at
the factory to be the same as the sensitivity for the x-axis,
the accelerometer can be programmed for non-equal
sensitivities on the x- and y-axes. Contact the factory for
additional information.
TOUT – This pin is the buffered output of the temperature
sensor. The analog voltage at TOUT is an indication of the
die temperature. This voltage is useful as a differential
measurement of temperature from ambient and not as an
absolute measurement of temperature. After correlating the
voltage at TOUT to 25°C ambient, the change in this
voltage due to changes in the ambient temperature can be
used to compensate for the change over temperature of the
accelerometer offset and sensitivity. Please refer to the
section on Compensation for the Change in Sensitivity
Over Temperature for more information.
Sck – The standard product is delivered with an internal
clock option (800kHz). This pin should be grounded
when operating with the internal clock. An external
clock option can be special ordered from the factory
allowing the user to input a clock signal between 400kHz
And 1.6MHz
Vref – This pin is the output of a reference voltage. It is set
at 2.50V typical and has 100μA of drive capability.
MEMSIC MXD2020E/F Rev H
COMPENSATION FOR THE CHANGE IN
SENSITIVITY OVER TEMPERATURE
All thermal accelerometers display the same sensitivity
change with temperature. The sensitivity change depends
on variations in heat transfer that are governed by the laws
of physics. Manufacturing variations do not influence the
sensitivity change, so there are no unit-to-unit differences
in sensitivity change. The sensitivity change is governed
by the following equation (and shown in Figure 1 in °C):
Sensitivity (normalized)
PIN DESCRIPTIONS
VDD – This is the supply input for the digital circuits and
the sensor heater in the accelerometer. The DC voltage
should be between 3.00 and 5.25 volts. Refer to the section
on PCB layout and fabrication suggestions for guidance on
external parts and connections recommended.
Page 4 of 8
In gaming applications where the game or controller is
typically used in a constant temperature environment,
sensitivity might not need to be compensated in hardware
or software. The compensation for this effect could be
done instinctively by the game player.
For applications where sensitivity changes of a few percent
are acceptable, the above equation can be approximated
with a linear function. Using a linear approximation, an
external circuit that provides a gain adjustment of –0.9%/°C
would keep the sensitivity within 10% of its room
temperature value over a 0°C to +50°C range.
For applications that demand high performance, a low cost
micro-controller can be used to implement the above
equation. A reference design using a Microchip MCU (p/n
16F873/04-SO) and MEMSIC developed firmware is
available by contacting the factory. With this reference
design, the sensitivity variation over the full temperature
range (-40°C to +105°C) can be kept below 3%. Please
visit the MEMSIC web site at www.memsic.com for
reference design information on circuits and programs
including look up tables for easily incorporating sensitivity
compensation.
DISCUSSION OF TILT APPLICATIONS AND
RESOLUTION
Tilt Applications: One of the most popular applications of
the MEMSIC accelerometer product line is in
tilt/inclination measurement. An accelerometer uses the
2/26/2007
force of gravity as an input to determine the inclination
angle of an object.
resolution of the measurement. With a simple RC low pass
filter, the rms noise is calculated as follows:
A MEMSIC accelerometer is most sensitive to changes in
position, or tilt, when the accelerometer’s sensitive axis is
perpendicular to the force of gravity, or parallel to the
Earth’s surface. Similarly, when the accelerometer’s axis is
parallel to the force of gravity (perpendicular to the Earth’s
surface), it is least sensitive to changes in tilt.
Noise (mg rms) = Noise(mg/ Hz ) * ( Bandwidth( Hz) *1.6)
Table 1 and Figure 2 to help illustrate the output changes in
the X- and Y-axes as the unit is tilted from +90° to 0°.
Notice that when one axis has a small change in output per
degree of tilt (in mg), the second axis has a large change in
output per degree of tilt. The complementary nature of
these two signals permits low cost accurate tilt sensing to
be achieved with the MEMSIC device (reference
application note AN-00MX-007).
X
M E M SIC
+90 0
gravity
0
0
Top View
Figure 2: Accelerometer Position Relative to Gravity
X-Axis
90
85
80
70
60
45
30
20
10
5
0
X Output
(g)
Change
per deg.
of tilt
(mg)
Y-Axis
Y Output
(g)
1.000
0.15
0.000
0.996
1.37
0.087
0.985
2.88
0.174
0.940
5.86
0.342
0.866
8.59
0.500
0.707
12.23
0.707
0.500
15.04
0.866
0.342
16.35
0.940
0.174
17.16
0.985
0.087
17.37
0.996
0.000
17.45
1.000
Table 1: Changes in Tilt for X- and Y-Axes
Change
per deg.
of tilt
(mg)
17.45
17.37
17.16
16.35
15.04
12.23
8.59
5.86
2.88
1.37
0.15
In many applications the microcontroller provides an
effective approach for the temperature compensation of the
sensitivity and the zero g offset. Specific code set, reference
designs, and applications notes are available from the
factory. The following parameters must be considered in a
digital interface:
DUTY CYCLE DEFINITION
The MXD2020E/F has two PWM duty cycle outputs (x,y).
The acceleration is proportional to the ratio T1/T2. The
zero g output is set to 50% duty cycle and the sensitivity
scale factor is set to 20% duty cycle change per g. These
nominal values are affected by the initial tolerance of the
device including zero g offset error and sensitivity error.
This device is offered from the factory programmed to
either a 10ms period (100 Hz) or a 2.5ms period (400Hz).
T1
T2 (Period)
Duty Cycle
Pulse width
Resolution: Accelerometers can be used in a wide variety
of low g applications such as tilt and orientation. The
device noise floor will vary with the measurement
bandwidth. With the reduction of the bandwidth the noise
floor drops. This will improve the signal to noise ratio of
the measurement and resolution. The output noise scales
directly with the square root of the measurement
bandwidth. The maximum amplitude of the noise, its peakto- peak value, approximately defines the worst case
MEMSIC MXD2020E/F Rev H
DIGITAL INTERFACE
The MXD2020E/F is easily interfaced with low cost
microcontroller. For the digital output accelerometer, one
digital input port is required to read one accelerometer
output. For the analog output accelerometer, many low cost
microcontroller are available today that feature integrated
a/d (analog to digital converters) with resolutions ranging
from 8 to 12 bits.
Resolution: smallest detectable change in input acceleration
Bandwidth: detectable accelerations in a given period of
time
Acquisition Time: the duration of the measurement of the
acceleration signal
Y
X-Axis
Orientation
To Earth’s
Surface
(deg.)
The peak-to-peak noise is approximately equal to 6.6 times
the rms value (for an average uncertainty of 0.1%).
Page 5 of 8
Length of the “on” portion of the cycle.
Length of the total cycle.
Ratio of the “0n” time (T1) of the cycle to
the total cycle (T2). Defined as T1/T2.
Time period of the “on” pulse. Defined as
T1.
T2
T1
A (g)= (T1/T2 - 0.5)/0.2
At 0g T1=T2
T2= 2.5ms or 10ms (factory programmable)
Figure 3: Typical output Duty Cycle
2/26/2007
CHOOSING T2 AND COUNTER FREQUENCY
DESIGN TRADE-OFFS
The noise level is one determinant of accelerometer
resolution. The second relates to the measurement
resolution of the counter when decoding the duty cycle
output. The actual resolution of the acceleration signal is
limited by the time resolution of the counting devices used
to decode the duty cycle. The faster the counter clock, the
higher the resolution of the duty cycle and the shorter the
T2 period can be for a given resolution. Table 2 shows
some of the trade-offs. It is important to note that this is the
resolution due to the microprocessors’ counter. It is
probable that the accelerometer’s noise floor may set the
lower limit on the resolution.
CounterResoCounts
Clock
MEMSIC
lution
Counts
Per T2
Rate
Sample
(mg)
per g
Cycle
(MHz)
Rate
T2 (ms)
10.0
100
1.0
10000
2000
0.5
10.0
100
0.5
5000
1000
1.0
2.5
400
1.0
2500
500
2.0
2.5
400
0.5
1250
250
4.0
Table 2: Trade-Offs Between Microcontroller Counter Rate and
T2 Period.
COMPENSATION FOR ZERO G OFFSET CHANGE
OVER TEMPERATURE
The compensation of offset is performed with the following
equation: Aoc = A + ( a + b * T + c * T * T)
where Aoc is the offset compensated acceleration, A is the
uncompensated acceleration, T is temperature and a, b, c
are constants characteristic to each accelerometer.
Computer programs are used to determine these constants.
The constants can be read from and written to the MCU
EEPROM via the RS-232. The constants a,b,c are normally
stored in the MCU EEPROM. To determine the values of
the constants, each accelerometer is taken to three different
temperatures, preferably evenly spread across the desired
temperature span. The zero g bias (A0, A1 and A2) and the
temperatures (T0, T1 and T2) are recorded at each
temperature. The data collected (A0, T0, A1, T1, A2, T2) is
used in a quadratic interpolation (or LaGrange polynomial)
to determine a, b and c as follows:
r0 = A0 / ( (T0-T1)*(T0-T2) )
r1 = A1 / ( (T1-T0)*(T1-T2) )
r2 = A2 / ( (T2-T0)*(T2-T1) )
a = r0 * T1 * T2 + r1 * T0 * T2 + r2 * T0 * T1
b = - r0 * (T1+T2) – r1 * (T0+T2) – r2 *(T0+T1)
c = r0 + r1 + r2
For a more detail discussion of temperature compensation
reference MEMSIC application note #AN-00MX-002
Microcontroller
MEMSIC
Accel
Ax
Ay
T
I/O
A/D
Figure 4: Zero g Offset Temperature Compensation Circuit
COMPENSATION FOR EXTENDING THE
FREQUENCY RESPONSE
The response of the thermal accelerometer is a function of
the internal gas physical properties, the natural convection
mechanism and the sensor electronics. Since the gas
properties of MEMSIC's mass produced accelerometer are
uniform, a digital filter can be used to equally compensate
all sensors. The compensating filter does not require
adjustment for individual accelerometers. The function of
the compensating filter is to apply gain in proportion with
the acceleration changes. The faster the acceleration
changes occur, the higher the gain that the filter applies.
For analog output accelerometers, the compensating filter
can be implemented with a circuit involving two op-amps
and some resistors and capacitors. For digital output
accelerometers, a digital filter is necessary.
In applications where high frequency accelerations need to
be measured, a DSP (digital signal processor) may be
necessary to implement the digital filter. DSP IC’s and
development tools are readily available from major IC
manufacturers.
However, if the bandwidth requirement is relatively low
(i.e. 100Hz), it is possible to implement a digital frequency
compensating filter with an 8 bit microcontroller. The
microcontroller will likely have to be capable of operating
at relatively high clock frequencies (20MHz).
CONVERTING THE DIGITAL OUTPUT TO AN
ANALOG OUTPUT
The PWM output can be easily converted into an analog
output by integration. A simple RC filter can do the
conversion. Note that that the impedance of the circuit
following the integrator must be much higher than the
impedance of the RC filter. Reference figure 5 for an
example.
10K
DOUT
In many cases a computer is used to control the
temperature, communicate with the MCU, and to calculate
the constants. After calculating the constants, the computer
downloads the constants to EEPROM.
I/O
MEMSIC
Accel.
AOUT
1uF
Figure 5: Converting the digital output to an analog voltage
MEMSIC MXD2020E/F Rev H
Page 6 of 8
2/26/2007
TEMPERATURE OUTPUT NOISE REDUCTION
It is recommended that a simple RC low pass filter is used
when measuring the temperature output. Temperature
output is typically a very slow changing signal, so a very
low frequency filter eliminates erroneous readings that may
result from the presence of higher frequency noise. A
simple filter is shown in Figure 6.
8.2K
TOUT
MEMSIC
Accel.
Power Supply
C1
0.1uF
VDA
VDD
MEMSIC
Accelerometer
Filtered TOUT
0.1uF
Figure 7: Power Supply Noise Rejection
Figure 6: Temperature Output Noise Reduction
POWER SUPPLY NOISE REJECTION
One capacitor is recommended for best rejection of power
supply noise (reference Figure 7 below). The capacitor
should be located as close as possible to the device supply
pin (VDD). The capacitor lead length should be as short as
possible, and surface mount capacitor is preferred. For
typical applications, the capacitor can be ceramic 0.1 μF.
MEMSIC MXD2020E/F Rev H
Page 7 of 8
PCB LAYOUT AND FABRICATION SUGGESTIONS
1. The Sck pin should be grounded to minimize noise.
2. Liberal use of ceramic bypass capacitors is
recommended.
3. Robust low inductance ground wiring should be used.
4. Care should be taken to ensure there is “thermal
symmetry” on the PCB immediately surrounding the
MEMSIC device and that there is no significant heat
source nearby.
5. A metal ground plane should be added directly beneath
the MEMSIC device. The size of the ground plane
should be similar to the MEMSIC device’s footprint
and be as thick as possible.
6. Vias can be added symmetrically around the ground
plane. Vias increase thermal isolation of the device
from the rest of the PCB.
2/26/2007
PACKAGE DRAWING
Fig 8: Hermetically Sealed Package Outline
MEMSIC MXD2020E/F Rev H
Page 8 of 8
2/26/2007