Complete rate gyroscope on a single chip
Z-axis (yaw-rate) response
High vibration rejection over wide frequency
2000 g powered shock survivability
Self-test on digital command
Temperature sensor output
Precision voltage reference output
Absolute rate output for precision applications
5 V single-supply operation
Ultra small and light (< 0.15 cc, < 0.5 gram)
APPLICATIONS
GPS navigation systems
Image stabilization
Inertial measurement units
Platform stabilization
FUNCTIONAL BLOCK DIAGRAM
–
+
5V
100nF100nF
AVCC
ST1
ST2
5G
4G
SELF
TEST
3A
RATE
SENSOR
2G1F
GENERAL DESCRIPTION
The ADXRS401 is a functionally complete and low cost angular
rate sensor (gyroscope), integrated with all of the required
electronics on one chip. It is manufactured using Analog
Devices’ surface-micromachining technique, the same high
volume BIMOS process used for high reliability automotive
airbag accelerometers. It is available in a 7 mm × 7 mm × 3 mm
BGA surface-mount package.
The output signal, RATEOUT (1B, 2A), is a voltage proportional
to angular rate about the axis normal to the top surface of the
package (see Figure 2). A single external resistor can be used to
lower the scale factor. An external capacitor is used to set the
bandwidth. Other external capacitors are required for operation
(see Figure 1).
A precision reference and a temperature output are also
provided for compensation techniques. Two digital self-test
inputs electromechanically excite the sensor to test proper
operation of both sensors and the signal conditioning circuits.
AGND
CORIOLIS SIGNAL CHANNEL
π
DEMOD
RESONATOR LOOP
≈
Gyro with Signal Conditioning
ADXRS401
C
OUT
SEN
SUMJ
1C
R
OUT
2
180kΩ 1%
1B
RATEOUT
2A
CMID
1D
R
SEN
9kΩ±35%≈9kΩ±35%
S
1
CHARGE PUMP/REG.
CP1
PDD
PGND
100nF
4A5A7E6G
CP2
22nF
ADXRS401
Rev. 0
Information furnished by Analog Devices is believed to be accurate and reliable.
However, no responsibility is assumed by Analog Devices for its use, nor for any
infringements of patents or other rights of third parties that may result from its use.
Specifications subject to change without notice. No license is granted by implication
or otherwise under any patent or patent rights of Analog Devices. Trademarks and
registered trademarks are the property of their respective owners.
SENSITIVITY Top view clockwise rotation is positive output
Dynamic Range
1
Scale Factor
Nonlinearity Best fit straight line 0.1 % of FS
NULL
Initial Null 2.50 V
Turn-On Time Power on to ± ½°/s of final 35 ms
Linear Acceleration Effect Any axis 0.2 °/s/g
NOISE PERFORMANCE
Rate Noise @ 10 Hz bandwidth 3 mV (rms)
FREQUENCY RESPONSE
3 dB Bandwidth2 (User Selectable) 22 nF as C
Sensor Resonant Frequency 14 kHz
SELF TEST
ST1 RATEOUT Response
3
ST2 RATEOUT Response3 ST2 pin from Logic 0 to 1 +800 mV
Logic 1 Input Voltage Standard high logic level definition 3.3 V
Logic 0 Input Voltage Standard low logic level definition 1.7 V
Input Impedance To common 50
TEMPERATURE SENSOR
V
at 298K 2.50 V
OUT
Max Current Load on Pin Source to common 50 µA
Scale Factor Proportional to absolute temperature 8.4 mV/K
OUTPUT DRIVE CAPABILITY
Output Voltage Swing I
Capacitive Load Drive 1000 pF
2.5 V REFERENCE
Voltage Value 2.5 V
Load Drive to Ground Source 200 µA
Load Regulation 0 < I
POWER SUPPLY
Operating Voltage Range 4.75 5.00 5.25 V
Quiescent Supply Current 6.0 8.0 mA
Dynamic range is the maximum full-scale measurement range possible, including output swing range, initial offset, sensitivity, offset drift, and sensitivity drift at 5 V
supplies.
2
Frequency at which response is 3 dB down from dc response with specified compensation capacitor value. Internal pole forming resistor is 180 kΩ. See the S
Bandwidth
3
Self-test response varies with temperature. See the section for details. Self-Test Function
section.
etting
Rev. 0 | Page 3 of 12
Page 4
ADXRS401
A
ABSOLUTE MAXIMUM RATINGS
Table 2.
Parameter Rating
Acceleration (Any Axis, Unpowered, 0.5 ms) 2000 g
Acceleration (Any Axis, Powered, 0.5 ms) 2000 g
+V
S
Output Short-Circuit Duration (Any Pin to
Common)
Operating Temperature Range
Storage Temperature
−0.3 V to +6.0 V
Indefinite
−55°C to +125°C
−65°C to +150°C
ESD CAUTION
ESD (electrostatic discharge) sensitive device. Electrostatic charges as high as 4000 V readily accumulate on
the human body and test equipment and can discharge without detection. Although this product features
proprietary ESD protection circuitry, permanent damage may occur on devices subjected to high energy
electrostatic discharges. Therefore, proper ESD precautions are recommended to avoid performance
degradation or loss of functionality.
Stresses above those listed under the Absolute Maximum
Ratings may cause permanent damage to the device. This is a
stress rating only; functional operation of the device at these or
any other conditions above those indicated in the operational
section of this specification is not implied. Exposure to absolute
maximum rating conditions for extended periods may affect
device reliability.
Applications requiring more than 200 cycles to MIL-STD-883
Method 1010 Condition B (–55°C to +125°C) require underfill
or other means to achieve this requirement.
Drops onto hard surfaces can cause shocks of greater than
2000 g and exceed the absolute maximum rating of the device.
Care should be exercised in handling to avoid damage.
RATE-SENSITIVE AXIS
This Z-axis rate-sensing device is also called a yaw-rate sensing
device. It produces a positive-going output voltage for clockwise
rotation about the axis normal to the package top (clockwise
when looking down at the package lid).
RATE
AXIS
LONGITUDINAL
AXIS
ABCDEFG
1
LATERAL AXIS
Figure 2. RATEOUT Signal Increases with Clockwise Rotation
Figure 8. 10 g Random Vibration in Package-Lateral Axis Orientation
PACKAGE LONGITUDINAL AXIS (1/60 SEC SAMPLE RATE)
2.50
04992-006
04992-007
30
25
20
15
% OF POPULATION
10
5
0
13.5014.0014.5015.0015.5016.0016.50
SENSITIVITY IN mV/DEGREE/SECOND
Figure 6. Initial Sensitivity
04992-005
Rev. 0 | Page 6 of 12
2.49
2.48
2.47
RATEOUT (V)
2.46
2.45
05
TIME (Seconds)
04992-008
10
Figure 9. 10 g Random Vibration in Package-Longitudinal Axis Orientation
Page 7
ADXRS401
2.50
RATE AXIS (1/60 SEC SAMPLE RATE)
2.50
PACKAGE LONGITUDINAL AXIS (0.5s AVERAGE)
2.49
2.48
2.47
RATEOUT (V)
2.46
2.45
05
TIME (Seconds)
Figure 10. 10 g Random Vibration in Rate Axis Orientation
PACKAGE LATERAL AXIS (0.5s AVERAGE)
0g
10g
RATEOUT (V)
2.50
2.49
2.48
2.47
2.46
04992-009
10
Figure 12. 10 g Random Vibration in Package-Longitudinal Axis Orientation
2.49
2.48
2.47
RATEOUT (V)
2.46
2.45
05
2.50
2.49
2.48
2.47
RATEOUT (V)
2.46
10g
0g
TIME (Seconds)
RATE AXIS (0.5s AVERAGE)
10g
0g
04992-011
10
2.45
05
TIME (Seconds)
10
Figure 11. 10 g Random Vibration in Package-Lateral Axis Orientation
04992-010
2.45
05
TIME (Seconds)
04992-012
10
Figure 13. 10 g Random Vibration in Rate Axis Orientation
Rev. 0 | Page 7 of 12
Page 8
ADXRS401
THEORY OF OPERATION
22nF
100nF
PGND
CP1
22nF
CP2
5V
AVCC
RATEOUT
CP4
7B
6A
5A
4A
3A
2A
1B
SUMJ
C
= 22nF
OUT
Figure 14. Example Application Circuit (Top View)
Note that inner rows/columns of pins have been omitted for clarity but should be connected in the application.
The ADXRS401 operates on the principle of a resonator gyro.
Two polysilicon sensing structures each contain a dither frame,
which is electrostatically driven to resonance. This produces the
necessary velocity element to produce a Coriolis force during
angular rate. At two of the outer extremes of each frame,
orthogonal to the dither motion, are movable fingers that are
placed between fixed pickoff fingers to form a capacitive pickoff
structure that senses Coriolis motion.
The resulting signal is fed to a series of gain and demodulation
stages that produce the electrical rate signal output. The dualsensor design rejects external g-forces and vibration.
Fabricating the sensor with the signal conditioning electronics
preserves signal integrity in noisy environments.
The electrostatic resonator requires 14 V to 16 V for operation.
Since only 5 V is typically available in most applications, a
charge pump is included on-chip. If an external 14 V to 16 V
supply is available, the two capacitors on CP1 to CP4 can be
omitted and this supply can be connected to CP5 (Pin 7D) with
a 1 µF decoupling capacitor.
After the demodulation stage there is a single-pole low-pass
filter consisting of an internal 9 kΩ resistor (R
) and an
SEN1
external user-supplied capacitor (CMID). A CMID capacitor of
100 nF sets a 400 Hz low-pass pole ± 35% and is used to limit
high frequency artifacts before final amplification. A bandwidth
limit capacitor, C
, sets the pass bandwidth (see Setting
OUT
Bandwidth section).
1µF
1E
PDD
2.5V
PGND
7F
1F
AGND
6G
5G
4G
3G
2G
CP4
ST1
ST2
TEMP
04992-013
CP5
CP3
7C
7D7E
100nF
1D
1C
CMID
100nF
SUPPLY AND COMMON CONSIDERATIONS
Only power supplies used for supplying analog circuits are
recommended for powering the ADXRS401. High frequency
noise and transients associated with digital circuit supplies may
have adverse affects on device operation. 1 µF shows the
recommended connections for the ADXRS401 where both
AVCC and PDD have a separate decoupling capacitor. These
should be placed as close to their respective pins as possible
before routing to the system analog supply. This will minimize
the noise injected by the charge pump that uses the PDD supply.
It is also recommended to place the charge pump capacitors
connected to the CP1 to CP4 pins as close to the part as
possible. These capacitors are used to produce the on-chip high
voltage supply switched at the dither frequency at
approximately 14 kHz. Care should be taken to ensure that
there is no more than 50 pF of stray capacitance between CP1
to CP4 and ground. Surface-mount chip capacitors are suitable
as long as they are rated for over 15 V.
Rev. 0 | Page 8 of 12
Page 9
ADXRS401
(
)
SETTING BANDWIDTH
External capacitors CMID and C
with on-chip resistors to create two low-pass filters to limit the
bandwidth of the ADXRS401’s rate response. The –3 dB
frequency set by R
OUT
and C
are used in combination
OUT
is:
OUT
INCREASING MEASUREMENT RANGE
To increase the full-scale measurement range of the ADXRS401,
place an external resistor between the RATEOUT (1B, 2A) and
SUMJ (1C, 2C) pins. This parallels the internal R
is factory-trimmed to 180 kΩ.
resistor that
OUT
CRπ21/f×××=
OUTOUTOUT
This frequency can be well controlled since R
has been
OUT
trimmed during manufacturing to be 180 kΩ ±1%. Any external
resistor applied between the RATEOUT (1B, 2A) and SUMJ
(1C, 2C) pins will result in:
R
OUT
()(
+×=
RkΩ180/RkΩ180
)
EXTEXT
The −3 dB frequency is set by RSEN (the parallel combination
and R
of R
SEN1
controlled, because R
) at about 4.5 kΩ nominal. CMID is less well
SEN2
SEN1
and R
have been used to trim the
SEN2
rate sensitivity during manufacturing and have a ±35%
tolerance. Its primary purpose is to limit the high frequency
demodulation artifacts from saturating the final amplifier stage.
Thus, this pole of nominally 400 Hz @ 0.1 µF need not be
precise. Lower frequency is preferable, but its variability usually
requires it to be about 10 times greater (in order to preserve
phase integrity) than the well-controlled output pole. In general,
both −3 dB filter frequencies should be set as low as possible to
reduce the amplitude of these high frequency artifacts, as well as
to reduce the overall system noise.
–
+
5V
100nF
AVCC
ST1
ST2
5G
4G
SELF
TEST
3A
RATE
SENSOR
2G1F
CORIOLIS SIGNAL CHANNEL
RESONATOR LOOP
AGND
π
DEMOD
For example, a 330 kΩ external resistor gives approximately
10mV/°/sec sensitivity and a commensurate ∼50% increase in
the full-scale range. This is effective for up to a 4× increase in
the full-scale range. (The minimum value of the parallel resistor
allowed is 45 kΩ.) Beyond this amount of external sensitivity
reduction, the internal circuitry headroom requirements
prevent further increase in the linear full-scale output range.
The drawbacks of modifying the full-scale range are the
additional output null drift (as much as 2°/sec over
temperature) and the readjustment of the initial null bias. See
Null Adjust section and Application Note AN-625 for details.
TEMPERATURE OUTPUT AND CALIBRATION
It is common practice to temperature-calibrate gyros to
improve their overall accuracy. The ADXRS401 has a
temperature-proportional voltage output that provides input to
such a calibration method. The voltage at TEMP (3F, 3G) is
nominally 2.5 V at 27°C and has a PTAT (proportional to
absolute temperature) characteristic of 8.4 mV/°C. Note that the
TEMP output circuitry is limited to 50 µA source current.
Limiting the bandwidth of the device reduces the flat-band
noise during the calibration process, improving the
measurement accuracy at each calibration point.
C
SUMJ
R
OUT
180kΩ 1%
OUT
1B
RATEOUT
2A
100nF
CMID
R
1
SEN
≈
9kΩ±35%≈9kΩ±35%
1D
1C
S
2
SEN
ADXRS401
CHARGE PUMP/REG.
4A5A7E6G
CP2
22nF
PDD
CP1
7F 6A7D7C7B
PGNDCP4
100nF
2.5V REF
PTAT
12V
CP3 CP5
1µF
22nF
1E
3G
2.5V
TEMP
04992-014
Figure 15. Block Diagram with External Components
Rev. 0 | Page 9 of 12
Page 10
ADXRS401
USE WITH A SUPPLY-RATIOMETRIC ADC
The ADXRS401’s RATEOUT signal is nonratiometric (that is,
neither the null voltage nor the rate sensitivity is proportional to
the supply). Rather, they are nominally constant for dc supply
changes within the 4.75 V to 5.25 V operating range. If the
ADXRS401 is used with a supply-ratiometric ADC, the
ADXRS401’s 2.5 V output can be converted and used to make
corrections in software for the supply variations.
NULL ADJUST
Null adjustment is possible by injecting a suitable current to
SUMJ (1C, 2C). Simply add a suitable resistor to either the
ground or the positive supply. The nominal 2.5 V null is for a
symmetrical swing range at RATEOUT (1B, 2A). In some
applications, a nonsymmetrical output swing may be suitable.
If a resistor is connected to the positive supply, supply
disturbances may reflect some null instability. Avoid digital
supply noise, particularly in this case (see the Supply and
Common Considerations section).
The resistor value to use is approximately:
×=
V
is the unadjusted zero rate output, and V
NULL0
null value. If the initial value is below the desired value, the
resistor should terminate on common or ground. If it is above
the desired value, the resistor should terminate on the 5 V
supply. Values typically are in the 1 MΩ to 5 MΩ range.
If an external resistor is used across RATEOUT and SUMJ, the
parallel equivalent value is substituted into the above equation.
Note that the resistor value is an estimate since it assumes
= 5.0 V and V
V
CC
SUMJ
= 2.5 V.
SELF-TEST FUNCTION
The ADXRS401 includes a self-test feature that stimulates each
of the sensing structures and associated electronics in the same
manner, as if subjected to angular rate. It is activated by
standard logic high levels applied to inputs ST1 (5F, 5G), ST2
(4F, 4G), or both. ST1 causes the voltage at RATEOUT to
change about −0.800 V, and ST2 causes an opposite +0.800 V.
Activating both ST1 and ST2 simultaneously is not damaging.
Because ST1 and ST2 are not necessarily closely matched,
actuating both simultaneously may result in an apparent null
bias shift.
)V – V180,000)/( (2.5 R
NULL1NULL0NULL
is the target
NULL1
ACCELERATION SENSITIVITY
The sign convention used is that lateral acceleration is positive
in the direction from Pin Column A to Pin Column G of the
package. That is, a device has positive sensitivity if its voltage
output increases when the row of Pins 2A to 6A are tipped
under the row 2G to 6G in the Earth’s gravity.
There are two effects of concern: shifts in the static null and
induced null noise. Scale factor is not significantly affected until
acceleration reaches several hundred meters per second
squared.
Vibration rectification for frequencies up to 20 kHz is of the
order of 0.00002(°/s)/(m/s
0.0003(°/s)/(m/s
2)2
the lid. It is not significantly dependent on frequency, and has
been verified up to 300 m/s
Linear vibration spectral density near the 14 kHz sensor
resonance translates into output noise. In order to have a
significant effect, the vibration must be within the angular rate
bandwidth (typically ±40 Hz of the resonance), so it takes
considerable high frequency vibration to have any effect.
Away from the 14 kHz resonance, the effect is not discernible,
except for vibration frequencies within the angular rate pass
band. The in-band effect can be seen in Figure 17. This is the
result of the static g-sensitivity. The specimen used for Figure 17
had a g-sensitivity of 0.15 °/s/g and its total in-band noise
degraded from 3 mV rms to 5 mV rms for the specified
vibration. The effect of broadband vibration up is shown in
Figure 18 and Figure 19.
The output noise of the part falls away in accordance with the
output low-pass filter and does not contain any spikes greater
than 1% of the low frequency noise. A typical noise spectrum is
shown in Figure 16.
–60
–70
–80
–90
–100
RATEOUT (V)
–110
2)2
in the primary axis and
for acceleration applied along a diagonal of
2
rms.
–120
–130
0101001k10k100k
Figure 16. Noise Spectral Density at RATEOUT – BW = 4Hz
FREQUENCY (Hz)
04992-015
Rev. 0 | Page 10 of 12
Page 11
ADXRS401
2.60
2.60
2.58
2.56
2.54
RATEOUT (V)
2.52
2.50
02468
TIME (Seconds)
Figure 17. Random Vibration (Lateral) 2 Hz to 40 Hz 3.2 g rms
2.60
2.58
2.56
2.54
RATEOUT (V)
2.52
04992-016
10
2.58
2.56
2.54
RATEOUT (V)
2.52
2.50
02468
STATIC 0.8mV rms
SHAKING 2.5mV rms
TIME (Seconds)
Figure 19. Random Vibration (Lateral) 10 kHz to 20 kHz
√
at 0.01 g/
0.07
0.06
0.05
0.04
/s
°
0.03
0.02
Hz with 60 Hz Sampling and 0.5 Sec Averaging
04992-018
10
0.01
0
010100
TIME (Seconds)
Figure 20. Root Allen Variance vs. Averaging Time
04992-019
2.50
02468
TIME (Seconds)
Figure 18. Random Vibration (Lateral) 10 kHz to 20 kHz