Datasheet AD2S105AP Datasheet (Analog Devices)

Page 1
Three-Phase
I
S1
Vds
Vqs
SECTOR
MULTIPLIER
SINE AND
COSINE
MULTIPLIER
INPUT DATA
STROBE
HOMOPOLAR
OUTPUT
HOMOPOLAR
REFERENCE
+5V GND –5V
φ
POSITION
PARALLEL
DATA
12 BITS
3
φ-2φ
Cos (θ + 120°)
Cos (θ + 240°)
SinθCosθ
Cosθ
Sinθ
Cos θ + φ
CONV1 CONV2
DECODE
BUSY
Vds'
Vqs'
Sin
θ + φ
SECTOR
MULTIPLIER
SINE AND
COSINE
MULTIPLIER
Ia + Ib + Ic
3
I
S2
I
S3
a
Transformation Three-Phase Balance Diagnostic–Homopolar Output DQ Manipulation Real-Time Filtering
APPLICATIONS AC Induction Motor Control Spindle Drive Control Pump Drive Control Compressor Drive Control and Diagnostics Harmonic Measurement Frequency Analysis Three-Phase Power Measurement
GENERAL DESCRIPTION
The AD2S105 performs the vector rotation of three-phase 120 degree or two-phase 90 degree sine and cosine signals by trans­ferring these inputs into a new reference frame which is controlled by the digital input angle φ. Two transforms are included in the AD2S105. The first is the Clarke transform which computes the sine and cosine orthogonal components of a three-phase in­put. These signals represent real and imaginary components which then form the input to the Park transform. The Park transform relates the angle of the input signals to a reference frame controlled by the digital input port. The digital input port on the AD2S105 is a 12-bit/parallel natural binary port.
If the input signals are represented by Vds and Vqs, respectively, where Vds and Vqs are the real and imaginary components, then the transformation can be described as follows:
Vds' = Vds Cosφ – Vqs Sinφ Vqs' = Vds Sinφ + Vqs Cosφ
Where Vds' and Vqs' are the output of the Park transform and Sinφ, and Cosφ are the trigonometric values internally cal­culated by the AD2S105 from the binary digital data φ.
The input section of the device can be configured to accept either three-phase inputs, two-phase inputs of a three-phase system, or two 90 degree input signals. The homopolar output indicates an imbalance of a three-phase input only at a user­specified level.
The digital input section will accept a resolution of up to 12 bits. An input data strobe signal is required to synchronize the position data and load this information into the device counters.
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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 which may result from its use. No license is granted by implication or otherwise under any patent or patent rights of Analog Devices.
Current Conditioner
AD2S105

FUNCTIONAL BLOCK DIAGRAM

A two-phase rotated output facilitates the implementation of multiple rotation blocks.
The AD2S105 is fabricated on LC ±5 volt power supplies.

PRODUCT HIGHLIGHTS

Current Conditioning
The AD2S105 transforms the analog stator current signals (I I
, I
) using the digital angular signal (reference frame) into dc
2
3
s
s
values which represent direct current (I rent (I
). This transformation of the ac signals into dc values
qs
simplifies the design of the analog-to-digital (A/D) conversion scheme. The A/D conversion scheme is simplified as the band­width sampling issues inherent in ac signal processing are avoided and in most drive designs, simultaneous sampling of the stator currents may not be necessary.
Hardware Peripheral for Standard Microcontroller and DSP Systems
The AD2S105 off-loads the time consuming Cartesian transfor­mations from digital processors and benchmarks show a signifi­cant speed improvement over single processor designs. AD2S105 transformation time = 2 µs.
Field Oriented Control of AC Motors
The AD2S105 accommodates all the necessary functions to pro­vide a hardware solution for current conditioning in variable speed control of ac synchronous and asynchronous motors.
Three-Phase Imbalance Detection
The AD2S105 can be used to sense imbalances in a three-phase system via the homopolar output.
One Technology Way, P.O. Box 9106, Norwood. MA 02062-9106, U.S.A. Tel: 617/329-4700 Fax: 617/326-8703
2
MOS and operates on
) and quadrature cur-
ds
,
s1
Page 2
(VDD = +5 V ± 5%; VSS = –5 V ± 5% AGND = DGND = O V;
AD2S105–SPECIFICATIONS
TA = –40°C to +85°C, unless otherwise noted)
Parameter Min Typ Max Units Conditions
SIGNAL INPUTS
PH/IP1, 2, 3, 4 Voltage Level ±2.8 ±3.3 V p-p DC to 50 kHz PH/IPH1, 2, 3 Voltage Level ±4.25 V p-p DC to 50 kHz Input Impedance
PH/IP1, 2, 3 7.5 10 k PH/IPH1, 2, 3 13.5 18 k PH/IP1, 4 1 M Mode 1 Only (2 Phase)
Sin & Cos
Gain
PH/IP1, 2, 3, 4 0.95 1 1.05 PH/IPH1, 2, 3 0.56
VECTOR PERFORMANCE
3-Phase Input-Output
Radius Error (Any Phase) ±0.4 ±1 % DC to 600 Hz Angular Error
1, 2
PH/IP 15 30 arc min DC to 600 Hz PH/IPH 30 arc min DC to 600 Hz
Differential Nonlinearity ±1 LSB Full Power Bandwidth 50 kHz Small Signal Bandwidth 200 kHz
ANALOG SIGNAL OUTPUTS
PH/OP1, 4 PH/IP, PH/IPH INPUTS
Output Voltage
3
±2.8 ±3.3 V p-p DC to 50 kHz
Offset Voltage 2 10 mV Inputs = 0 V Slew Rate 2 V/µs Small Signal Step Response 1 µs1° Input to Settle to
±1 LSB (Input to Output)
Output Impedance 15 Output Drive Current 3.0 4.0 mA Outputs to AGND Resistive Load 2 k Capacitive Load 50 pF
STROBE
Write 100 ns Positive Pulse Max Update Rate 366 kHz
BUSY
Pulse Width 1.7 2.5 µs Conversion in Process V
OH
V
OL
4V dcI
1V dcI
= 0.5 mA
OH
= 0.5 mA
OL
DIGITAL INPUTS
DB1–DB12
V
IH
V
IL
Input Current, I
IN
Input Capacitance, C
IN
3.5 V dc
1.5 V dc ±10 µA
10 pF
CONV MODE
(CONV1, CONV2)
V
IH
V
IL
3.5 V dc
1.5 V dc
Input Current 100 µA Internal 50 k Input Capacitance 10 pF Pull-Up Resistor
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AD2S105
WARNING!
ESD SENSITIVE DEVICE
Parameter Min Typ Max Units Conditions
HOMOPOLAR OUTPUT
HPOP–OUTPUT
V
OH
V
OL
HPREF–REFERENCE 0.5 V dc Homopolar Output-Internal
POWER SUPPLY
V
DD
V
SS
I
DD
I
SS
NOTES
1
Angular accuracy includes offset and gain errors, measured with a stationary digital input and maximum analog frequency inputs.
2
The angular error does not include the additional error caused by the phase delay as a function of input frequency. For example, if f
to the error due to phase delay is: 650 ns × f
3
Output subject to input voltage and gain.
Specifications subject to change without notice.
× 60 × 360 = 8.4 arc minutes.
INPUT
4V dcI
1V dcI
= 0.5 mA
OH
= 0.5 mA
OL
I
= 25 µA and 20 k to AGND
SOURCE
4.75 5 5.25 V dc –5.25 –5 –4.75 V dc
4 10 mA Quiescent Current 4 10 mA Quiescent Current
= 600 Hz, the contribution
INPUT

RECOMMENDED OPERATING CONDITIONS

Power Supply Voltage (+VDD, –V
) . . . . . . . . . ±5 V dc ± 5%
SS
Analog Input Voltage (PH/IP1, 2, 3, 4) . . . . . . 2 V rms ± 10%
Analog Input Voltage (PH/IPH1, 2, 3) . . . . . . 3 V rms ± 10%
Ambient Operating Temperature Range
Industrial (AP) . . . . . . . . . . . . . . . . . . . . . . .–40°C to +85°C

ABSOLUTE MAXIMUM RATINGS (TA = +25°C)

VDD to AGND . . . . . . . . . . . . . . . . . . . . . . . –0.3 V to +7 V dc
V
to AGND . . . . . . . . . . . . . . . . . . . . . . . +0.3 V to –7 V dc
SS
AGND to DGND . . . . . . . . . . . . . . . . . . . . . . . . . . . ±0.3 V dc
Analog Input Voltage to AGND . . . . . . . . . . . . . . . V
Digital Input Voltage to DGND . . . . –0.3 V to V
Digital Output Voltage to DGND . . . . . . –0.3 V to V
to V
SS
+ 0.3 V dc
DD
DD
DD
+ V dc
Analog Output Voltage to AGND
. . . . . . . . . . . . . . . . . . . . . . V
– 0.3 V to VDD + 0.3 V dc
SS
Analog Output Load Condition (PH/OP1, 4
Sinθ, Cosθ) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2 k
Power Dissipation . . . . . . . . . . . . . . . . . . . . . . . . . . . .140 mW
Operating Temperature
Industrial (AP) . . . . . . . . . . . . . . . . . . . . . . . –40°C to +85°C
Storage Temperature . . . . . . . . . . . . . . . . .–65°C to +150°C
Lead Temperature (Soldering, 10 sec) . . . . . . . . . . . . . +300°C
CAUTION
1. Absolute Maximum Ratings are those values beyond which damage to the device will occur.
2. Correct polarity voltages must be maintained on the +V
DD
and –VSS pins

ORDERING GUIDE

Model Temperature Range Accuracy Option*
AD2S105AP –40°C to +85°C 30 arc min P-44A
*P = Plastic Leaded Chip Carrier.
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 the AD2S105 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.
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AD2S105
6 5 4 3 2 1 44 43 42 41 40
18 19 20 21 22 23 24 25 26 27 28
29
30
31
32
33
34
35
36
37
38
39
V
SS
V
DD
STROBE
NC
NC
BUSY
DGND
V
DD
NC
NC
V
SS
HPREF
HPOP
CONV1
CONV2
COS
DB12
HPFILT
DB11
NC = NO CONNECT.
TOP VIEW
(NOT TO SCALE)
AD2S105
PH/OP4
NC
SIN
7
8
11
12
13
14
15
16
17
9
10
NC
DB1
DB2
DB3
DB4
DB5
DB6
DB7
DB8
DB9
DB10
PH/OP1
NC
NC
AGND
PH/IP4
PH/IPH3
PH/IP3
PH/IPH2
PH/IP2
PH/IPH1
PH/IP1
PIN DESIGNATIONS
1, 2, 3
Pin Mnemonic Description
3 STROBE Begin Conversion 4V 5V
DD SS
Positive Power Supply Negative Power Supply
6 PH/OP4 Sin (θ + φ) 7 PH/OP1 Cos (θ + φ) 10 AGND Analog Ground 11 PH/IP4 Sin θ Input 12 PH/IPH3 High Level Cos
(θ + 240°) Input
13 PH/IP3 Cos (θ + 240°) Input 14 PH/IPH2 High Level Cos
(θ + 120°) Input 15 PH/IP2 Cos (θ + 120°) Input 16 PH/IPH1 High Level Cos θ Input 17 PH/IP1 Cos (θ) Input 19 V
SS
Negative Power Supply 20 HPREF Homopolar Reference 21 HPOP Homopolar Output 22 HPFILT Homopolar Filter 23 CONV1 Select Analog Input
Format 24 CONV2 Select Analog Input
Format 25 COS Cos Output 26 SIN Sin Output 27–38 DB12 to DB1 (DB1 = MSB, DB12 =
LSB Parallel Input Data) 41 V
DD
Positive Power Supply 42 DGND Digital Ground 44 BUSY Internal Logic Setup
Time
NOTES
1
90° orthogonal signals = Sin θ, Cos θ (Resolver) = PH/IP4 and PH/IP1.
2
Three phase, 120°, three-wire signals = Cos θ, Cos (θ + 120°), Cos (θ + 240°).
= PH/IP1, PH/IP2, PH/IP3 High Level = PH/IPH1, PH/IPH2, PH/IPH3.
3
Three Phase, 120°, two-wire signals = Cos (θ + 120°), Cos (θ + 240°) =
PH/IP2, PH/IP3. In all cases where any of the input Pins 11 through 17 are not used, they must be left unconnected.
PIN CONFIGURATION
–4–
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AD2S105
I
ds
I
qs
Ids'
I
qs
'
φ
e
j
φ
THEORY OF OPERATION
A fundamental requirement for high quality induction motor drives is that the magnitude and position of the rotating air-gap rotor flux be known. This is normally carried out by measuring the rotor position via a position sensor and establishing a rotor oriented reference frame.
To generate a flux component in the rotor, stator current is ap­plied. A build-up of rotor flux is concluded which must be maintained by controlling the stator current, i
, parallel to the
ds
rotor flux. The rotor flux current component is the magnetizing current, i
mr
.
Torque is generated by applying a current component which is perpendicular to the magnetizing current. This current is nor­mally called the torque generating current, i
qs
.
To orient and control both the torque and flux stator current vectors, a coordinate transformation is carried out to establish a new reference frame related to the rotor. This complex calcula­tion is carried out by the AD2S105.
To expand upon the vector operator a description of a single vector rotation is of assistance. If it is considered that the moduli of a vector is OP and that through the movement of ro­tor position by f, we require the new position of this vector it can be deduced as follows:
Let original vector OP = A (Cos u + jSIN u) where A is a constant;
if OQ = OP e and: e
jF
jF
= Cos f + jSin f
(1)
OQ = A (Cos (u + f) + jSin (u + f))
= A [Cos u Cos φSin u Sin φ + jSin u Cos φ + jCos u Sin φ]
= A [(Cos u + jSin u) (Cos f + jSin f)] (2)
a
Q
θ + φ
φ
O
P
θ
d
To relate these stator current to the reference frame the rotor currents assume the same rectangular coordinates, but are now rotated by the operator e
jf
, where ejf = Cos f + jSin f.
Here the term vector rotator comes into play where the stator current vector can be represented in rotor-based coordinates or vice versa.
The AD2S105 uses e mathematical function, it rotates the orthogonal i
jf
as the core operator. In terms of the
and iqs com-
ds
ponents as follows:
i
' + jiqs' = (Ids + jIqs) e
ds
jf
where ids', iqs' = stator currents in the rotor reference frame. And
jf
= Cos f + jSin f
e
+ jIqs)(Cos f + jSin f)
= (I
ds
The output from the AD2S105 takes the form of:
' = Ids Cos f – Iqs Sin f
i
ds
' = Ids Sin f + Iqs Cos f
i
qs
The matrix equation is:
ids']
[
iqs'
Cos f – Sin f
=
[
Sin f
Cos f I
I
ds
][
]
qs
and it is shown in Figure 2.
Figure 2. AD2S105 Vector Rotation Operation
INPUT CLARK
COSθ COSθ + 120° COS θ + 240°
SINθ
3φ TO 2φ
TRANSFORMATION
PARK
SINE AND
COSINE
MULTIPLIER
(DAC)
SINE AND
COSINE
MULTIPLIER
(DAC)
COS (θ + φ)
SIN (θ + φ)
Figure 1. Vector Rotation in Polar Coordinate
The complex stator current vector can be represented as is = i
+ aibs + a2ics where a = e
j2π
3
and a2 = e
j4π
. This can be re-
3
as
placed by rectangular coordinates as
In this equation i
= ids + ji
i
s
and iqs represent the equivalent of a two-
ds
qs
(3)
phase stator winding which establishes the same magnitude of MMF in a three-phase system. These inputs can be seen after the three-phase to two-phase transformation in the AD2S105
LATCH
DIGITAL
LATCH
φ
LATCH
Figure 3. Converter Operation Diagram
block diagram. Equation (3) therefore represents a three-phase to two-phase conversion.
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AD2S105

CONVERTER OPERATION

The architecture of the AD2S105 is illustrated in Figure 3. The AD2S105 is configured in the forward transformation which ro­tates the stator coordinates to the rotor reference frame.
Vector Rotation
Position data, f, is loaded into the input latch on the positive edge of the strobe pulse. (For detail on the timing, please refer to the “timing diagram.”) The negative edge of the strobe signi­fies that conversion has commenced. A busy pulse is subse­quently produced as data is passed from the input latches to the Sin and Cos multipliers. During the loading of the multiplier, the busy pulse remains high preventing further updates of f in both the Sin and Cos registers.
The negative edge of the busy pulse signifies that the multipliers are set up and the orthogonal analog inputs are then multiplied real time. The resultant two outputs are accessed via the PH/OP1 (Pin 7) and PH/OP4 (Pin 6).
For other configurations, please refer to “Transformation Configuration.”
CONNECTING THE CONVERTER Power Supply Connection
The power supply voltages connected to VDD and VSS pins should be +5 V dc and –5 V dc and must not be reversed. Pin 4 (V
) and Pin 41 (VDD) should both be connected to +5 V;
DD
similarly, Pin 5 (V
) and Pin 19 (VSS) should both be con-
SS
nected to –5 V dc. It is recommended that decoupling capacitors, 100 nF (ceramic)
and 10 µF (tantalum) or other high quality capacitors, are con- nected in parallel between the power line V
, VSS and AGND
DD
adjacent to the converter. Separate decoupling capacitors should be used for each converter. The connections are shown in Fig­ure 4.
+5V
DD
V
AD2S105
TOP VIEW
1
23
DD
V
GND
10µF
–5V
10µF
SS
100nF
+
+
100nF
V
AGND
12 34
SS
V
Figure 4. AD2S105 Power Supply Connection
ANALOG SIGNAL INPUT AND OUTPUT CONNECTIONS Input Analog Signals
All analog signal inputs to AD2S105 are voltages. There are two different voltage levels of three-phase (0°, 120°, 240°) signal in­puts. One is the nominal level, which is ± 2.8 V dc or 2 V rms and the corresponding input pins are PH/IP1 (Pin 17), PH/IP2 (Pin 15), PH/IP3 (Pin 13) and PH/IP4 (Pin 11).
The high level inputs can accommodate voltages from nominal up to a maximum of ±V
. The corresponding input pins
DD/VSS
are PH/IPH1 (Pin 16), PH/IPH2 (Pin 14) and PH/IPH3 (Pin
12). The homopolar output can only be used in the three-phase connection mode.
The converter can accept both two-phase format and three­phase format input signals. For the two-phase format input, the two inputs must be orthogonal to each other. For the three­phase format input, there is the choice of using all three inputs or using two of the three inputs. In the latter case, the third in­put signal will be generated internally by using the information of other two inputs. The high level input mode, however, can only be selected with three-phase/three-input format. All these different conversion modes, including nominal/high input level and two/three-phase input format can be selected using two se­lect pins (Pin 23, Pin 24). The functions are summarized in Table I.
Table I. Conversion Mode Selection
CONV1 CONV2
Mode Description (Pin 23) (Pin 24)
MODE1 2-Phase Orthogonal with 2 Inputs NC DGND
Nominal Input Level
MODE2 3-Phase (0°, 120°, 240°) with 3 Inputs DGND V
Nominal/High Input Level*
MODE3 3-Phase (0°, 120°, 240°) with 2 Inputs V
Nominal Input Level
*The high level input mode can only be selected with MODE2.
DD
DD
V
DD
MODE1: 2-Phase/2 Inputs with Nominal Input Level
In this mode, PH/IP1 and PH/IP4 are the inputs and the Pins 12 through 16 must be left unconnected.
MODE2: 3-Phase/3 Inputs with Nominal/High Input Level
In this mode, either nominal or high level inputs can be used. For nominal level input operation, PH/IP1, PH/IP2 and PH/IP3 are the inputs, and there should be no connections to PH/IPH1, PH/IPH2 and PH/IPH3; similarly, for high level input opera­tion, the PH/IPH1, PH/IPH2 and PH/IPH3 are the inputs, and there should be no connections to PH/IP1, PH/IP2 and PH/IP3. In both cases, the PH/IP4 should be left unconnected. For high level signal input operation, select MODE2 only.
MODE3: 3-Phase/2 Inputs with Nominal Input Level
In this mode, PH/IP2 and PH/IP3 are the inputs and the third signal will be generated internally by using the information of other two inputs. It is recommended that PH/IP1, PH/IPH1, PH/IPH2, PH/IP4 and PH/IPH3 should be left unconnected.
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AD2S105
Output Analog Signals
There are two sets of analog output from the AD2S105. Sin/Cos orthogonal output signals are derived from the Clark/
three-to-two-phase conversion before the Park angle rotation. These signals are available on Pin 25 (Cos u) and Pin 26 (Sin u), and occur before Park angle rotation.
Two-Phase (Sin (u + f), Cos (u + f)) Signals
These represent the output of the coordinate transformation. These signals are available on Pin 6 (PH/OP4, Sin (u + f)) and Pin 7 (PH/OP1, Cos (u + f)).
HOMOPOLAR OUTPUT HOMOPOLAR Reference
In a three-phase ac system, the sum of the three inputs to the converter can be used to indicate whether or not the phases are balanced.
If V
= PH/IP1 + PH/IP2 + PH/IP3 (or PH/IPH1 + PH/
SUM
IPH2 + PH/IPH3) this can be rewritten as V
= [Cosu, +
SUM
Cos (u + 120°) + Cos (u + 240°)] = 0. Any imbalances in the line will cause the sum V output (HPOP) goes high when V
0. The AD2S105 homopolar
SUM
SUM
> 3 × V
. The voltage
ts
level at which the HPOP indicates an imbalance is determined by the HPREF threshold, V
. This is set internally at ±0.5 V dc
ts
(±0.1 V dc). The HPOP goes high when
(Cosθ+Cos(θ+120°)+ Cos(θ+240°))
Vts<
3
×V
where V is the nominal input voltage. With no external components V
must exceed ±1.5 V dc in
SUM
order for HPOP to indicate an imbalance. The sensitivity of the threshold can be reduced by connecting an external resistor be­tween HPOP and ground in Figure 5 where
0.5 R
EXT
EXT
+20,000
R
EXT
is in .
Vts=
R
Example: From the equivalent circuit, it can be seen that the in­clusion of a 20 k resistor will reduce V
to ±0.25 V dc. This
ts
corresponds to an imbalance of ±0.75 V dc in the inputs.
Homopolar Filtering
The equation V = 0 denotes an imbalance when V
= Cosu + Cos (u + 120°) + Cos (u + 240°)
SUM
0. There are conditions,
SUM
however, when an actual imbalance will occur and the condi­tions as defined by V
will be valid. For example, if the first
SUM
phase was open circuit when u = 90° or 270°, the first phase is valid at 0 V dc. V
is valid, therefore, when Cosu is close to 0.
SUM
In order to detect an imbalance u has to move away from 90° or 270°, i.e., when on a balanced line Cos u 0.
Line imbalance is detected as a function of HPREF, either set by the user or internally set at ± 0.5 V dc. This corresponds to a dead zone when f = 90° or 270° ± 30°, i.e., V
= 0, and,
SUM
therefore, no indicated imbalance. If an external 20 k resistor is added, this halves V
and reduces the zone to ±15°. Note this
ts
example only applies if the first phase is detached. In order to prevent this false triggering an external capacitor
needs to be placed from HPFILT to ground, as shown in Figure
5. This averages out the perceived imbalance over a complete cycle and will prevent the HPOP from alternatively indicating balance and imbalance over u = 0° to 360°.
For
dθ
=1000 rpm C
dt
dθ
=100 rpm C
dt
EXT
EXT
= 220 nF
= 2. 2 µF
Note: The slower the input rotational speed, the larger the time constant required over which to average the HPOP output. Use of the homopolar output at slow rotational speeds becomes im­practical with respect to the increased value for C
34
EXT
.
25µA
HOMOPOLAR
REFERENCE
EXTERNAL RESISTOR
TO TRIGGER
20k
Figure 5. The Equivalent Homopolar Reference Input Circuitry
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–7–
DGND
AD2S105
TOP VIEW
1
HPFILT
HPOP
HPREF
AGND
12
C
EXT
23
220nF
HPOP HPREF
R
EXT
GND
Figure 6. AD2S105 Homopolar Output Connections
Page 8
AD2S105
THREE PHASE INPUT
AD2S105
TOP VIEW
141
38
30
27
23
12
16
DIGITAL ANGLE INPUT
LSB
SIN
COS
10µF
100nF
10µF100nF
–5V
+5V
GND
TWO PHASE OUTPUT
STROBE
BUSY
HPOP
HPFILT
HPREF
MSB
PH/OP1
AGND PH/IP4
PH/IP3
PH/IP2
PH/IP1
34
TIMING DIAGRAMS Busy Output
The BUSY output will go HI at the negative edge of the STROBE input. This is used to synchronize digital input data and load the digital angular rotation information into the device counter. The BUSY output will remain HI for 2 µs, and go LO until the next strobe negative edge occurs.
Strobe Input
The width of the positive STROBE pulse should be at least 100 ns, in order to successfully start the conversion. The maxi­mum frequency of STROBE input is 366 kHz, i.e., there should be at least 2.73 µs from the negative edge of one STROBE pulse to the next rising edge. This is illustrated by the following tim­ing diagram and table.
t
STROBE
BUSY
t
1
t
2
t
r
4
t
f
t
3
Figure 7. AD2S105 Timing Diagram
Note: Digital data should be stable 25 ns before and after posi­tive strobe edge.
Table II. AD2S105 Timing Table
Parameter Min Typ Max Condition
t
1
t
2
t
3
t
4
t
r
100 ns STROBE Pulse Width
30 ns STROBE to BUSY
1.7 µs 2.5 µs BUSY Pulse Width 100 ns BUSY to STROBE 20 ns BUSY Pulse Rise Time
with No Load
150 ns BUSY Pulse Rise Time
with 68 pF Load
t
f
10 ns BUSY Pulse Fall Time
with No Load
120 ns BUSY Pulse Fall Time
with 68 pF Load

TYPICAL CIRCUIT CONFIGURATION

Figure 8 shows a typical circuit configuration for the AD2S105 in a three phase, nominal level input mode (MODE2).
Figure 8. Typical Circuit Configuration
APPLICATIONS Transformation Configuration
The AD2S105 can perform both forward and reverse transfor­mations. The section “Theory of Operation” explains how the chip operates with the core operator e ward transformation. The reverse transformation, e
+jf
, which performs a for-
–jf
, is per-
formed by providing a negative angle φ. Figure 9 shows two different phase input/output connections for AD2S105 reverse transformation operation.
2 PHASE – 2 PHASE
3 PHASE – 2 PHASE
Figure 9. Forward and Reverse Transformation Connections
FORWARD
TRANSFORMATION
AD2S105
Cosθ Cos(θ + φ)
Sinθ
Cosθ
Cos(θ + 120°) Cos(θ + 240°)
REVERSE
TRANSFORMATION
AD2S105
+j
φ
e
Sin(θ + φ)
Cos(θ + φ)
+j
φ
e
Sin(θ + φ)
Cosθ
Sinθ
Cosθ
Cos(θ + 120°) Cos(θ + 240°)
–j
φ
e
–j
φ
e
–8–
Cos(θ φ)
Sin(θ φ)
Cos(θ φ) Sin(θ φ)
–1
REV. 0
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AD2S105

MEASUREMENT OF HARMONICS

In ac power systems, the quality of the electrical supply can be affected by harmonic voltages injected into the power main by loads, such as variable speed drive systems and computer power supplies. These harmonics are injected into other loads through the point of common coupling of the supply. This produces ex­tra losses in power factor correction capacitors, power supplies and other loads which may result in failure. It also can result in tripping and failure of computer systems and other sensitive equipment. In ac machines the resultant harmonic currents and flux patterns produce extra motor losses and torque pulsations, which can be damaging to the load.
The AD2S105 can be used to monitor and detect the presence and magnitude of a particular harmonic on a three-phase line. Figure 10 shows the implementation of such a scheme using the AD2S105, where Va, Vb, Vc are the scaled line voltages.
Va Vb
TRANSFORMATION
Vc
AD2S105
THREE -TO-TWO
CLARK
HOMOPOLAR
OUTPUT
Vd
TRANSFORMATION
Vq
12-BIT UP/DOWN
COUNTER
jφ
PARK
e
1
Vd
LOW PASS
1
Vq
PULSE INPUTS
DIRECTION
FILTER
a
k
Figure 10. Harmonics Measurement Using AD2S105
Selecting a harmonic is achieved by synchronizing the rotational frequency of the park digital input, f, with the frequency of the fundamental component and the integer harmonic selected. The update rate, r, of the counters is determined by:
r = 4096 ×
n ×ω
2π
.
Here, r = input clock pulse rate (pulses/second);
n = the order of harmonics to be measured; v = fundamental angular frequency of the ac signal.
The magnitude of the n-th harmonic as well as the fundamental component in the power line is represented by the output of the low-pass filter, a
. In concert with magnitude of the harmonic
k
the AD2S105 homopolar output will indicate whether the three
phases are balanced or not. For more details about this applica­tion, refer to the related application note listed in the bibliography.

Field Oriented Control of AC Induction Motors

In ac induction motors, torque is produced through interaction between the rotating air gap field and currents induced in the rotor windings. The stator currents consist of two components, the flux component which drives the air gap field, and the torque component which is reflected from the rotor windings. A successful field oriented control strategy must independently control the flux component of current, referred to as direct cur­rent (I rent, referred to as quadrature current (I
), and the torque producing component of stator cur-
ds
qs
).
The control architecture in Figure 11 is referred to as field ori­ented because the control algorithms performed on the ADSP­2105 processor operate on decoupled flux and torque current components in a reference frame relative to the rotor flux of the motor. The control algorithms provide fast torque response at any speed which results in superior dynamic performance, and consequently, load variations have minimal effect on speed or position control.
The AD2S90 resolver-to-digital converter is used to convert the modulated resolver position signals into a 12-bit digital position value. This value is brought into the ADSP-2105 via the serial port where the control algorithms calculate the rotor flux angle. The rotor flux angle is the sum of the rotor position and the slip angle. The relationship between the stator current fre­quency and the slip frequency can be summarized by the follow­ing formula:
f
where: f
= (vm × (p/2)) + f
stat
= Stator Current Frequency (Hz)
s
tat
s
lip
vm = Mechanical Speed of the Motor ( revs/sec )
p = Number of poles f
= Slip Frequency (Hz)
s
lip
The rotor flux angle is fed into the 12-bit position input of the AD2S105. The AD2S105 transforms the three ac stator cur­rents using the digital rotor flux angle into dc values represent­ing direct current (I
) and quadrature current (Iqs). The
ds
transformation of the ac signals into dc values simplifies the de­sign of the A/D converter as it avoids the bandwidth sampling issues inherent in ac signal processing and in most cases elimi­nates the need for a simultaneous sampling A/D converter.
REV. 0
STATOR
CURRENT
SIGNALS
Ids
I
s1
I
s2
I
s3
AD2S105
2 CHANNEL
12 Bit A/D
CONVERTER
Iqs
ROTOR FLUX ANGLE
ADSP-2105
ROTOR
FLUX
MODEL
SPORT
ROTOR POSITION DATA
INV
+
PWM
MOTOR
AD2S90
R / D
CONVERTER
RESOLVER
Figure 11. Field Oriented Control of AC Induction Motors
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AD2S105
AD2S80A
AD2S105
BIT1 BIT2 . . . . . . BIT13 BIT14
MSB MSB-1 . . . . . . . LSB
(MSB)
(LSB)
14-BIT RESOLUTION MODE
. . . . . .

MULTIPLE POLE MOTORS

For multi-pole motor applications where a single speed resolver is used, the AD2S105 input has to be configured to match the electrical cycle of the resolver with the phasing of the motor windings. The input to the AD2S105 is the output of a resolver­to-digital converter, e.g., AD2S80A series. The parallel output of the converter needs to be multiplied by 2
n–1
, where n = the number of pole pairs of the motor. In practice this is imple­mented by shifting the parallel output of the converter left rela­tive to the number of pole pairs. This will work for motors with a binary number of pole pairs.
Figure 12 shows the generic configuration of the AD2S80A with the AD2S105 for a motor with n pole pairs. The MSB of the AD2S105 is connected to MSB–(n–1) bit of the AD2S80A digi­tal output, MSB-1 bit to MSB–(n–2) bit, etc.
AD2S80A AD2S105
MSB MSB-1 . . . MSB – (n–1) . . .
12,14 OR 16-BIT RESOLUTION MODE
n = POLES
. . . .
MSB MSB-1 MSB-2 . . . . . . .
Figure 12. A General Consideration in Connecting R/D Converter and AD2S105 for Multiple Pole Motors
Figure 13 shows the AD2S80A configured for use with a four pole motor, where n = 2. Using the formula described the MSB is shifted left once.
Figure 13. Connecting of R/D Converter AD2S80A and AD2S105 for Four-Pole Motor Application

APPLICATION NOTES LIST

1. “Vector Control Using a Single Vector Rotation Semicon­ductor for Induction and Permanent Magnet Motors,” by F.P. Flett, Analog Devices.
2. “Silicon Control Algorithms for Brushless Permanent Mag­net Synchronous Machines,” by F.P. Flett.
3. “Single Chip Vector Rotation Blocks and Induction Motor Field Oriented Control,” by A.P.M. Van den Bossche and P.J.M. Coussens.
4. “Three Phase Measurements with Vector Rotation Blocks in Mains and Motion Control,” P.J.M. Coussens, et al.
5. “A Tutorial in AC Induction and Permanent Magnet Synchronous Motors–Vector-Control with Digital Signal Processors.
–10–
REV. 0
Page 11
OUTLINE DIMENSIONS
Dimensions shown in inches and (mm).
44-Lead Plastic Leaded Chip Carrier (P-44A)
0.180 (4.57)
0.165 (4.19)
40
39
29
28
0.048 (1.21)
0.042 (1.07)
0.020
(0.50)
0.048 (1.21)
0.042 (1.07)
6
7
17
18
R
PIN 1
IDENTIFIER
TOP VIEW
0.656 (16.66)
0.650 (16.51)
0.695 (17.65)
0.685 (17.40)
0.056 (1.42)
0.042 (1.07)
SQ
SQ
0.110 (2.79)
0.085 (2.16)
0.025 (0.63)
0.015 (0.38)
0.021 (0.53)
0.013 (0.33)
0.63 (16.00)
0.59 (14.99)
0.032 (0.81)
0.026 (0.66)
0.050 (1.27) BSC
0.040 (1.01)
0.025 (0.64)
AD2S105
REV. 0
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C1938–18–7/94
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PRINTED IN U.S.A.
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