AD2S1200
Rev. 0 | Page 9 of 24
PRINCIPLE OF OPERATION
The AD2S1200 operates on a Type II tracking closed-loop
principle. The output continually tracks the position of the
resolver without the need for external convert and wait states.
As the resolver moves through a position equivalent to the least
significant bit weighting, the output is updated by one LSB.
The converter tracks the shaft angle θ by producing an output
angle ϕ that is fed back and compared to the input angle θ, and
the resulting error between the two is driven towards 0 when
the converter is correctly tracking the input angle. To measure
the error, S3–S1 is multiplied by Cosϕ and S2–S4 is multiplied
by Sinϕ to give
42
31
0
0
StoSSinCostSinE
StoSCosSintSinE
φθω
φθω
×
×
The difference is taken, giving
)(
0
φ
θ
φ
θ×ω SinCosCosSintSinE
Equation 2.
This signal is demodulated using the internally generated
synthetic reference, yielding
)(
0
φθφθ
SinCosCosSinE
Equation 3.
Equation 3 is equivalent to E
0
Sin (θ ϕ), which is
approximately equal to E
0
(θ ϕ) for small values of θ ϕ,
where
θ ϕ = angular error.
The value E
0
(θ ϕ) is the difference between the angular error
of the rotor and the converter’s digital angle output.
A phase-sensitive demodulator, integrators, and a compensation
filter form a closed-loop system that seeks to null the error
signal. When this is accomplished, ϕ equals the resolver angle θ
within the rated accuracy of the converter. A Type II tracking
loop is used so that constant velocity inputs can be tracked
without inherent error.
For more information about the operation of the converter, see
the Circuit Dynamics section.
FAULT DETECTION CIRCUIT
The AD2S1200 fault detection circuit will detect loss of resolver
signals, out of range input signals, input signal mismatch, or loss
of position tracking. In these cases, the position indicated by the
AD2S1200 may differ significantly from the actual shaft
position of the resolver.
Monitor Signal
The AD2S1200 generates a monitor signal by comparing the
angle in the position register to the incoming Sin and Cos
signals from the resolver. The monitor signal is created in a
similar fashion to the error signal described in the Principle of
Operation section. The incoming signals Sin
θ and Cosθ are
multiplied by the Sin and Cos of the output angle, respectively,
and then added together as shown below:
φ
×
θ
×+
φ
θ
×
=
CosCosASinxSinAMonitor 21
Equation 4.
Where A1 is the amplitude of the incoming Sin signal (A1 ×
Sin
θ), A2 is the amplitude of the incoming Cos signal (A2 ×
Cos
θ), θ is the resolver angle, and ϕ is the angle stored in the
position register. Note that Equation 4 is shown after demodula-
tion, with the carrier signal Sin
ωt removed. Also note that for
matched input signal (i.e., no-fault condition), A1 = A2.
When A1 = A2 and the converter is tracking (
θ = ϕ), the
monitor signal output has a constant magnitude of A1 (Monitor
= A1 × (Sin
2
θ + Cos
2
θ) = A1), independent of shaft angle.
When A1
A2, the monitor signal magnitude varies between
A1 and A2 at twice the rate of shaft rotation. The monitor signal
is used as described in the following sections to detect
degradation or loss of input signals.
Loss of Signal Detection
Loss of signal (LOS) is detected when either resolver input (Sin
or Cos) falls below the specified LOS Sin/Cos threshold by
comparing the monitor signal to a fixed minimum value. LOS is
indicated by both DOS and LOT latching as logic low outputs.
The DOS and LOT pins are reset to the no fault state by a rising
edge of
SAMPLE
. The LOS condition has priority over both the
DOS and LOT conditions, as shown in Table 4. LOS is indicated
within 45° of angular output error worst case.
AD2S1200
Rev. 0 | Page 10 of 24
Signal Degradation Detection
Degradation of signal (DOS) is detected when either resolver
input (Sin or Cos) exceeds the specified DOS Sin/Cos threshold
by comparing the monitor signal to a fixed maximum value.
DOS is also detected when the amplitude of the input signals
Sin and Cos mismatch by more than the specified DOS Sin/
Cos mismatch by continuously storing the minimum and
maximum magnitude of the monitor signal in internal registers,
and calculating the difference between the minimum and
maximum. DOS is indicated by a logic low on the DOS pin, and
is not latched when the input signals exceed the maximum
input level. When DOS is indicated due to mismatched signals,
the output is latched low until a rising edge of
SAMPLE
resets
the stored minimum and maximum values. The DOS condition
has priority over the LOT condition, as shown in Table 4. DOS
is indicated within 30° of angular output error worst case.
Loss of Position Tracking Detection
Loss of tracking (LOT) is detected for three separate conditions:
When the internal error signal of the AD2S1200 has
exceeded 5°
When the input signal exceeds the maximum tracking rate
of 60,000 rpm (1,000 rps)
When the internal position (at the position integrator)
differs from the external position (at the position register)
by more than 5°
LOT is indicated by a logic low on the LOT pin, and is not
latched. LOT has a 4° hysteresis, and is not cleared until the
internal error signal or internal/external position mismatch is
less than 1°. When the maximum tracking rate is exceeded, LOT
is cleared when both the velocity is less than 1,000 rps and the
internal/external position mismatch is less than 1°. LOT can be
indicated for step changes in position (such as after a
RESET
signal is applied to the AD2S1200), or for accelerations
>~85,000 rps
2
. LOT is useful as a built-in test (BIT) that the
tracking converter is functioning properly. The LOT condition
has lower priority than both the DOS and LOS conditions as
shown in Table 4. The LOT and DOS conditions cannot be
indicated at the same time.
Table 4. Fault Detection Decoding
Condition DOS LOT Priority
Loss of Signal 0 0 1
Degradation of Signal 0 1 2
Loss of Tracking 1 0 3
No Fault 1 1
Responding to a Fault Condition
If any fault condition (LOS, DOS, or LOT) is indicated by the
AD2S1200, the output data must be presumed to be invalid.
This means that even if a
RESET
or
SAMPLE
pulse releases the
fault condition, the output data may be corrupted, even though
a fault may not be immediately indicated after the
RESET
/
SAMPLE
event. As discussed earlier, there are some fault
conditions with inherent latency. If the device fault is cleared,
there could be some latency in the resolver’s mechanical
position before the fault condition is re-indicated.
When a fault is indicated, all output pins will still provide data,
although the data may or may not be valid. The fault condition
will not force the parallel, serial, or encoder outputs to a known
state. However, a new startup sequence is recommended only
after a LOS fault has been indicated.
Response to specific fault conditions is a system-level
requirement. The fault outputs of the AD2S1200 indicate that
the device has sensed a potential problem with either the
internal or external signals of the AD2S1200. It is the
responsibility of the system designer to implement the
appropriate fault-handling schemes within the control hardware
and/or algorithm of a given application based on the indicated
fault(s) and the velocity or position data provided by the
AD2S1200.
False Null Condition
Resolver-to-digital converters that employ Type II tracking
loops based on the error equation (Equation 3) presented in the
Principle of Operation section can suffer from a condition
known as “false null. This condition is caused by a metastable
solution to the error equation when θ − ϕ = 180°. The
AD2S1200 is not susceptible to this condition because its
hysteresis is implemented externally to the tracking loop.
Because of the loop architecture chosen for the AD2S1200, the
internal error signal always has some movement (1 LSB per
clock cycle), and so, in a metastable state, the converter will
always move to an unstable condition within one clock cycle,
causing the tracking loop to respond to the false null condition
as if it were a 180° step change in input position (the response
time is the same as specified in Dynamic Performance section
of Table 1). Therefore, it is impossible to enter the metastable
condition any time after the startup sequence as long as the
resolver signals are valid. However, in a case of a loss of signal, a
full reset is recommended to avoid the possibility of a false null
condition. The response to the false null condition has been
included in the value of t
TRACK
provided in the Supply
Sequencing and Reset section.
AD2S1200
Rev. 0 | Page 11 of 24
CONNECTING THE CONVERTER
Refer to Figure 5. Ground should be connected to the AGND
pin and DGND pin. Positive power supply V
DD
= +5 V dc ± 5%
should be connected to the AV
DD
pin and DV
DD
pin. Typical
values for the decoupling capacitors are 10 nF and 4.7 µF,
respectively. These capacitors should be placed as close to the
device pins as possible, and should be connected to both AV
DD
and DV
DD
. If desired, the reference oscillator frequency can be
changed from the nominal value of 10 kHz using FS1 and FS2.
Typical values for the oscillator decoupling capacitors are 20 pF.
Typical values for the reference decoupling capacitors are 10 µF
and 0.01 µF, respectively.
04406-0-005
DV
DD
5V
1
2
3
4
5
6
7
8
9
10
11
RESET
33
32
31
30
29
28
27
26
25
24
DGND
8.912
MHz
20pF20pF
4.7µF 10nF
23
12 13 14 15
DGND
16
DV
DD
17 18 19 20 21 22
44
REFBYP
43
AGND
42
Cos
41
CosLO
40
AV
DD
39
SinLO
38
Sin
37
AGND
36 35
EXC
34
AD2S1200
EXC
10µF
10nF
5V
S2
S6
S3 S1
4.7µF
10nF
5V
BUFFER
CIRCUIT
BUFFER
CIRCUIT
R2
R1
Figure 5. Connecting the AD2S1200 to a Resolver
The gain of the buffer depends on the type of resolver used.
Since the specified excitation output amplitudes are matched to
the specified Sin/Cos input amplitudes, the gain of the buffer is
determined by the attenuation of the resolver.
In this recommended configuration, the converter introduces a
V
REF
/2 offset in the Sin, Cos signals coming from the resolver.
Of course, the SinLO and CosLO signals may be connected to a
different potential relative to ground, as long as the Sin and Cos
signals respect the recommended specifications. Note that since
the EXC/
EXC
outputs are differential, there is an inherent gain
of.
For example, if the primary to secondary turns ratio is 2:1, the
buffer will have unity gain. Likewise, if the turns ratio is 5:1, the
gain of the buffer should be 2.5×. Figure 6 suggests a buffer
circuit. The gain of the circuit is
)1/2( RRGain =
and
×
+×=
INREF
OUT
V
R
R
R
R
VV
1
2
1
2
1
V
REF
is set so that V
OUT
is always a positive value, eliminating the
need for a negative supply.
04406-0-006
12V
EXC/EXC
(V
IN
)
5V
(V
REF
)
R2
12V
V
OUT
33
33
R1
442 1.24k
12V
2.7k
2.7k
Figure 6. Buffer Circuit
Separate screened twisted cable pairs are recommended for
analog inputs Sin/SinLO and Cos/CosLO. The screens should
terminate to REFOUT. To achieve the dynamic performance
specified, an 8.192 MHz crystal must be used.

AD2S1200WSTZ

Mfr. #:
Manufacturer:
Analog Devices Inc.
Description:
Data Acquisition ADCs/DACs - Specialized IC12-Bit R/D Cnvtr w/Ref Oscillator
Lifecycle:
New from this manufacturer.
Delivery:
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