Data Sheet ADXRS649
Rev. B | Page 9 of 12
THEORY OF OPERATION
The ADXRS649 operates on the principle of a resonator gyro.
Figure 18 shows a simplified version of one of four polysilicon
sensing structures. Each sensing structure contains a dither
frame that is electrostatically driven to resonance. This pro-
duces the necessary velocity element to produce a Coriolis force
when experiencing angular rate. The ADXRS649 is designed to
sense a z-axis (yaw) angular rate.
When the sensing structure is exposed to angular rate, the result-
ing Coriolis force couples into an outer sense frame, which
contains movable fingers that are placed between fixed pickoff
fingers. This forms 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 quad sensor design rejects linear and angular
acceleration, including external g-forces and vibration. This is
achieved by mechanically coupling the four sensing structures
such that external g-forces appear as common-mode signals
that can be removed by the fully differential architecture
implemented in the ADXRS649.
The electrostatic resonator requires 13 V to 15 V for operation.
Because only 5 V are typically available in most applications,
a charge pump is included on chip. If an external 13 V to 15 V
supply is available, the two capacitors on CP1 to CP4 can be
omitted, and this supply can be connected to CP5 (Pin D6,
Pin D7). CP5 should not be grounded when power is applied
to the ADXRS649. No damage occurs, but under certain condi-
tions, the charge pump may fail to start up after the ground is
removed without first removing power from the ADXRS649.
SETTING THE BANDWIDTH
External Capacitor C
OUT
is used in combination with the on-
chip R
OUT
resistor to create a low-pass filter to limit the bandwidth
of the ADXRS649 rate response. The −3 dB frequency set by
R
OUT
and C
OUT
is
f
OUT
= 1/(2 × π × R
OUT
× C
OUT
)
f
OUT
can be well controlled because R
OUT
has been trimmed
during manufacturing to be 180 kΩ ± 1%. Any external resistor
applied between the RATEOUT pin (B1, A2) and the SUMJ pin
(C1, C2) results in
R
OUT
= (180 kΩ × R
EXT
)/(180 kΩ + R
EXT
)
In general, an additional filter (in either hardware or software)
is added to attenuate high frequency noise arising from demodu-
lation spikes at the 18 kHz resonant frequency of the gyro. An
RC output filter consisting of a 3.3 kΩ series resistor and 22 nF
shunt capacitor (2.2 kHz pole) is recommended.
X
Y
Z
09573-018
Figure 18. Simplified Gyro Sensing StructureOne Corner
ADXRS649 Data Sheet
Rev. B | Page 10 of 12
TEMPERATURE OUTPUT AND CALIBRATION
It is common practice to temperature-calibrate gyros to improve
their overall accuracy. The ADXRS649 has a temperature propor-
tional voltage output that provides input to such a calibration
method. The temperature sensor structure is shown in Figure 19.
The temperature output is characteristically nonlinear, and any
load resistance connected to the TEMP output results in decreasing
the TEMP output and its temperature coefficient. Therefore,
buffering the output is recommended.
The voltage at TEMP (F3, G3) is nominally 2.5 V at 25°C, and
V
RATIO
= 5 V. The temperature coefficient is ~9 mV/°C at 25°C.
Although the TEMP output is highly repeatable, it has only
modest absolute accuracy.
V
RATIO
TEMP
R
FIXED
R
TEMP
09573-019
Figure 19. Temperature Sensor Structure
MODIFYING THE MEASUREMENT RANGE
The ADXRS649 scale factor can be reduced to extend the
measurement range to as much as ±50,000°/sec by adding a
single 120 kΩ resistor between the RATEOUT and SUMJ pins.
If an external resistor is added between RATEOUT and SUMJ,
C
OUT
must be proportionally increased to maintain correct
bandwidth.
NULL BIAS ADJUSTMENT
The nominal 2.5 V null bias is for a symmetrical swing range at
RATEOUT (B1, A2). However, a nonsymmetric output swing
may be suitable in some applications. Null bias adjustment is
possible by injecting a suitable current to SUMJ (C1, C2). Note
that supply disturbances may reflect some null bias instability.
Digital supply noise should be avoided, particularly in this case.
SELF-TEST FUNCTION
The ADXRS649 includes a self-test feature that actuates each of
the sensing structures and associated electronics in the same
manner, as if subjected to angular rate. The self-test is activated
by standard logic high levels applied to Input ST1 (F5, G5),
Input ST2 (F4, G4), or both. ST1 causes the voltage at RATEOUT
to change by approximately −0.15 V, and ST2 causes an opposite
change of +0.15 V. The self-test response follows the viscosity
temperature dependence of the package atmosphere,
approximately 0.25%/°C.
Activating ST1 and ST2 simultaneously does not damage the
part. ST1 and ST2 are fairly closely matched (±2%), but
actuating both simultaneously may result in a small apparent
null bias shift proportional to the degree of self-test mismatch.
ST1 and ST2 are activated by applying a voltage equal to V
RATIO
to the ST1 pin and the ST2 pin. The voltage applied to ST1 and
ST2 must never be greater than AV
CC
.
CONTINUOUS SELF-TEST
The on-chip integration of the ADXRS649 gives it higher reliability
than is obtainable with any other high volume manufacturing
method. In addition, it is manufactured under a mature BiMOS
process that has field-proven reliability. As an additional failure
detection measure, a power-on self-test can be performed. How-
ever, some applications may warrant continuous self-test while
sensing rate. Information about continuous self-test techniques
is also available in the AN-768 Application Note, Using the
ADXRS150/ADXRS300 in Continuous Self-Test Mode.
Data Sheet ADXRS649
Rev. B | Page 11 of 12
OUTLINE DIMENSIONS
A
B
C
D
E
F
G
76543
TOP VIEW
DETAIL A
BALL DIAMETER
0.60
0.55
0.50
0.60 MAX
0.25 MIN
COPLANARITY
0.15
21
*
A1 CORNER
INDEX AREA
3.20 MAX
2.50 MIN
*
BALL A1 IDENTIFIER IS GOLD PLATED AND CONNECTED
TO THE D/A PAD INTERNALLY VIA HOLES.
10-26-2009-B
7.05
6.85 SQ
6.70
A1 BALL
CORNER
BOTTOM VIEW
DETAIL A
0.80
BSC
4.80
BSC SQ
SEATING
PLANE
3
.80 MAX
Figure 20. 32-Lead Ceramic Ball Grid Array [CBGA]
(BG-32-3)
Dimensions shown in millimeters
ORDERING GUIDE
Model
1
Temperature Range Package Description Package Option
ADXRS649BBGZ-RL –40°C to +105°C 32-Lead Ceramic Ball Grid Array [CBGA] BG-32-3
ADXRS649BBGZ –40°C to +105°C 32-Lead Ceramic Ball Grid Array [CBGA] BG-32-3
EVAL-ADXRS649Z Evaluation Board
1
Z = RoHS Compliant Part.

ADXRS649BBGZ

Mfr. #:
Manufacturer:
Analog Devices Inc.
Description:
Gyroscopes Vibrtion Reject Rate 20,000 Deg/s
Lifecycle:
New from this manufacturer.
Delivery:
DHL FedEx Ups TNT EMS
Payment:
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