Datasheet MC10E197FNR2, MC10E197FN Datasheet (Motorola)

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
SEMICONDUCTOR TECHNICAL DATA
2–1
REV 2
Motorola, Inc. 1996
12/93
 
The MC10E197 is an integrated data separator designed for use in high speed hard disk drive applications. With data rate capabilities of up to 50Mb/s the device is ideally suited for today’s and future state-of-the-art hard disk designs.
The E197 is typically driven by a pulse detector which reads the magnetic information from the storage disk and changes it into ECL pulses. The device is capable of operating on both 2:7 and 1:7 RLL coding schemes. Note that the E197 does not do any decoding but rather prepares the disk data for decoding by another device.
For applications with higher data rate needs, such as tape drive systems, the device accepts an external VCO. The frequency capability of the integrated VCO is the factor which limits the device to 50Mb/s.
A special anti-equivocation circuit has been employed to ensure timely lock-up when the arriving data and VCO edges are coincident.
Unlike the majority of the devices in the ECLinPS family, the E197 is available in only 10H compatible ECL. The device is available in the standard 28-lead PLCC.
Since the E197 contains both analog and digital circuitry, separate supply and ground pins have been provided to minimize noise coupling inside the device. The device can operate on either standard negative ECL supplies or, as is more common, on positive voltage supplies.
2:7 and 1:7 RLL Format Compatible
Fully Integrated VCO for 50Mb/s Operation
External VCO Input for Higher Operating Frequency
Anti-equivocation Circuitry to Ensure PLL Lock
INTERNAL
VCO
DATA
PHASE
DETECTOR
ACQUISITION
CIRCUITRY
CHARGE
PUMP
CURRENT-
SOURCES
PHASE DETECTOR MUX
PHASE FREQUENCY
DETECTOR
LOGIC DIAGRAM
RDEN
REFCLK
VCOIN
EXTVCO
ENVCO
RAWD
ACQ TYPE
CAP1 CAP2
PUMPUP PUMPDN RSETUP
RSETDN
RDATA RDCLK
VCO MUX
CLOCK &
DATA
BUFFER
This document contains information on a new product. Specifications and information herein are subject to change without notice.

DATA SEPARATOR
FN SUFFIX
PLASTIC PACKAGE
CASE 776-02
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MC10E197
MOTOROLA ECLinPS and ECLinPS Lite
DL140 — Rev 4
2–2
CAP1
CAP2
VCOIN
V
RSETUP
PUMPDN
RAWD
RAWD
Pinout: 28-Lead PLCC (Top View)
25 24 23 22 21 20 19
18 17
16 15
14 13 12
5 6 7 8 9 10 11
26 27
28
2 3 4
RDCLK RDCLK V
CC
RSDATA
RSDATA PUMPUP
RSETDN
TEST
EXTVCO
ENVCO
V
EE
ACQ
TYPE
RDEN
NC
RFFCLK
RFFCLK
CCO1
V
CCO0
V
CCVCO
V
CCVCO
1
PIN DESCRIPTIONS
REFCLK Reference clock equivalent to one clock cycle per decoding window. RDEN Enable data synchronizer when HIGH. When LOW enable the phase/frequency detector steered by REFCLK. RAWD Data Input to Synchronizer logic. VCOIN VCO control voltage input CAP1/CAP2 VCO frequency controlling capacitor inputs ENVCO VCO select pin. LOW selects the internal VCO and HIGH selects the external VCO input. Pin floats LOW when left open. EXTVCO External VCO pin selected when ENVCO is HIGH ACQ Acquisition circuitry select pin. This pin must be driven HIGH at the end of the data sync field for some sync field types. TYPE Selects between the two types of commonly used sync fields. When LOW it selects a sync field interspersed with 3 zeroes
(2:7 RLL code). When HIGH it selects a sync field interspersed with 2 zeroes (1:7 RLL code). TEST Input included to initialize the clock flip-flop for test purposes only. Pin should be left open (LOW) in actual application. PUMPUP Open collector charge pump output for the signal pump PUMPDN Open collector charge pump output for the reference pump RSETUP Current setting resistor for the signal pump RSETDN Current setting resistor for the reference pump RDATA Synchronized data output RDCLK Synchronized clock output VCC, V
CCO
,
V
CCVCO
Most positive supply rails. Digital and analog supplies are independent on chip
VEE, V
EEVCO
Most negative supply rails. Digital and analog supplies are independent on chip
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DC CHARACTERISTICS (VEE = VEE(min) to VEE(max); VCC = GND or VCC = 4.75V to 5.25V; VEE = GND)
0°C 25°C 85°C
Symbol Characteristic min typ max min typ max min typ max Unit Condition
I
IH
Input HIGH Current 150 150 150 µA 1
I
IL
Input LOW Current 0.5 0.5 0.5 µA 1
I
EE
Power Supply Current 90 150 180 90 150 180 90 150 180 mA
I
SET
Charge Pump Bias Current 0.5 5 0.5 5 0.5 5 mA 2
I
OUT
Charge Pump Output 1 1 1 µA 3 Leakage Current
V
ACT
PUMPUP/PUMPDN VCC– 2.5 V
CCVCC
– 2.5 V
CCVCC
– 2.5 V
CC
V
Active Voltage Range
10H LOGIC LEVELS DC CHARACTERISTICS (VEE = VEE(min) to VEE(max); VCC = V
CCO
+ V
CCO1
= V
CCVCO
= GND)
0°C 25°C 85°C
Symbol Characteristic min typ max min typ max min typ max Unit Condition
V
OH
Output HIGH Voltage –1020 – 840 – 980 – 810 – 910 –720 mV
V
OL
Output LOW Voltage –1950 –1630 –1950 –1630 –1950 –1595 mV
V
IH
Input HIGH Voltage –1170 –840 –1130 – 810 –1060 –720 mV
V
IL
Input LOW Voltage –1950 –1480 –1950 –1480 –1950 –1445 mV
POSITIVE EMITTER COUPLED LOGIC LEVELS DC CHARACTERISTICS (VEE = V
EEVCO
= GND; VCC = V
CCO1
= V
CCVCO
= +5 volts*)
0°C 25°C 85°C
Symbol Characteristic min typ max min typ max min typ max Unit Condition
V
OH
Output HIGH Voltage 3980 4160 4020 4190 4090 4280 mV
V
OL
Output LOW Voltage 3050 3370 3050 3370 3050 3405 mV
V
IH
Input HIGH Voltage 3830 4160 3870 4190 3940 4280 mV
V
IL
Input LOW Voltage 3050 3520 3050 3050 3050 3555 mV
1. *VOH and VOL levels will vary 1:1 with V
CC
AC CHARACTERISTICS (VEE = VEE(min) to VEE(max); VCC = GND or VCC = 4.75V to 5.25V; VEE = GND)
0°C 25°C 85°C
Symbol Characteristic min max min max min max Unit Condition
t
s
Time from RDATA Valid to Rising Edge of RDCLK
T
VCO
– 550 T
VCO
– 500 T
VCO
– 500 ps 4,7
t
H
Time from Rising Edge of RDCLK to RDATA invalid
T
VCO
T
VCO
T
VCO
ps 4,7
t
SKEW
Skew Between RDATA and RDATA
300 300 300 ps
f
VCO
Frequency of the VCO 150 150 150 MHz 5 Tuning Ratio 1.53 1.87 1.53 1.87 1.53 1.87 6
1. Applies to the input current for each input except VCOIN
2. For a nominal set current of 3.72mA, the resistor values for RSETUP and RSETDN should be 130(0.1%). Assuming no variation between these two resistors, the current match between the PUMPUP and PUMPDN output signals should be within ±3%. I
SET
is calculated as (VEE+
1.3v – VBE)/R; where R is RSETUP or RSETDN and a nominal value for VBE is 0.85 volts.
3. Output leakage current of the PUMPUP or PUMPDN output signals when at a LOW level.
4. T
VCO
is the period of the VCO.
5. The VCO frequency determined with VCOIN = VEE + 0.5 volts and using a 10pF tuning capacitor.
6. The tuning ratio is defined as the ratio of f
VCOMAX
to F
VCOMIN
where f
VCOMAX
is measured at VCOIN = 1.3V + VEE and f
VCOMAX
is measured
at VCOIN = 2.6V + VEE.
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2–4
RDATA
RDATA
RDCLK
RDCLK
t
S
t
H
SETUP AND HOLD TIMING DIAGRAMS
APPLICATIONS INFORMATION
General Operation
Operation
The E197 is a phase-locked loop circuit consisting of an internal VCO, a Data Phase detector with associated acquisition circuitry, and a Phase/Frequency detector (Figure
1). In addition, an enable pin(ENVCO) is provided to disable the internal VCO and enable the external VCO input. Hence, the user has the option of supplying the VCO signal.
The E197 contains two phase detectors: a data phase detector for synchronizing to the non-periodic pulses in the read data stream during the data read mode of operation, and a phase/ frequency detector for frequency (and phase) locking to an external reference clock during the “idle” mode of operation. The read enable (RDEN) pin muxes between these two detectors.
Data Read Mode
The data pins (RAWD) are enabled when the RDEN pin is placed at a logic high level, thus enabling the Data Phase detector (Figure1) and initiating the data read mode. In this mode, the loop is servoed by the timing information taken from the positive edges of the input data pulses. This phase detector samples positive edges from the RAWD signal and generates both a pump up and pump down pulse from any edge of the input data pulse. The leading edge of the pump up pulse is time modulated by the leading edge of the data signal, whereas the rising edge of the pump up pulse is generated synchronous to the VCO clock. The falling edge of the pump down pulse is synchronous to the falling edge of the VCO clock and the rising edge of the pump down signal is synchronous to the rising edge of the VCO clock. Since both edges of the VCO are used the internal clock a duty cycle of 50%. This pulse width modulation technique is used to generate the servoing signal which drives the VCO. The pump down signal is a reference pulse which is included to provide an evenly balanced differential system, thereby allowing the synthesis of a VCO input control signal after appropriate signal processing by the loop filter.
By using suitable external filter circuitry, a control signal for input into the VCO can be generated by inverting the pump down signal, summing the inverted signal with the pump up signal and averaging the result. The polarity of this control signal is defined as zero when the data edges lead the clock by a half clock cycle. If the data edges are advanced with respect to the zero polarity data/VCO edge relationship, the control signal is defined to have a negative polarity; whereas if the VCO is advanced with respect to the zero polarity data/VCO edge relationship, the control signal is defined to have a positive polarity . If there is no data edge present at the RAWD input, the corresponding pump up and pump down outputs are not generated and the resulting control output is zero.
Acquisition Circuitry
The acquisition circuitry is provided to assist the data phase detector in phase locking to the sync field that precedes the data. For the case in which lock-up is attempted when the data edges are coincident with the VCO edges, the pump down signal may enter an indeterminate state for an unacceptably long period due to the violation of internal set up and hold times. After an initial pump down pulse, the circuit blocks successive pump down pulses, and inserts extra pump up pulses, during portions of the sync field that are known to contain zeros. Thus, the data phase detector is forced to have a nonzero output during the lock-up period, and the restoring force ensures correction of the loop within an acceptable time. Hence, this circuitry provides a quasi-deterministic pump down output signal, under the condition of coincident data and VCO edges, allowing lock-up to occur with excessive delays.
The ACQ
line is provided to disable (disable = HIGH) the acquisition circuit during the data portion of a sector block. Typically, this circuit is enabled at the beginning of the sync field by a one-shot timer to ensure a timely lock-up.
The TYPE line allows the choice between two sync field preamble types; transitions interspersed with two zeros between transitions. These types of sync fields are used with the 1:7 and 2:7 coding schemes, respectively.
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Idle Mode
In the absence of data or when the drive is writing to the disk, PLL servoing is accomplished by pulling the read enable line (RDEN) low and providing a reference clock via the REFCLK pins. The condition whereby RDEN is low selects the Phase/Frequency detector (Figure 1) and the 10E197 is said to be operating in the “idle mode”. In order to function as a frequency detector the input waveform must be periodic. The pump up and pump down pulses from the Phase/Frequency detector will have the same frequency , phase and pulse width only when the two clocks that are being compared have their positive edges aligned and are of the same frequency.
As with the data phase detector, by using suitable external filter circuitry, a VCO input control signal can be generated by inverting the pump down signal, summing the inverted signal with the pump up signal and averaging the result. The polarity
of this control signal is defined as zero when all positive edges of both clocks are coincident. For the case in which the frequencies of the two clocks are the same but the clock edges of the reference clock are slightly advanced with respect to the VCO clock, the control clock is defined to have a positive polarity. A control signal with negative polarity occurs when the edges of the reference clock are delayed with respect to those of the VCO. If the frequencies of the two clocks are different, the clock with the most edges per unit time will initiate the most pulses and the polarity of the detector will reflect the frequency error. Thus, when the reference clock is high in frequency than the VCO clock the polarity of the control signal is positive; whereas a control signal with negative polarity occurs when the frequency of the reference clock is lower than the VCO clock.
Phase-Lock Loop Theory
Introduction
Phase lock loop (PLL) circuits are fundamentally feedback systems used to synchronize the frequency of an oscillator to an incoming signal. In addition to frequency synchronization, the PLL circuitry is designed to minimize the phase difference between the system input and output signals. A block diagram of a feedback control system is shown in Figure 1.
where:
A(s) is the product of the feed-forward transfer functions.
Figure 1. Feedback System
Xi(s) Xo(s)
A(s)
β
(s)
+
Xe(s)
R
β(s) is the product of the feedback transfer functions.
The transfer function for this closed loop system is
Xo(s) Xi(s)
=
A(s)
1 + A(s)β(s)
Typically, phase lock loops are modeled as feedback systems connected in a unity feedback configuration (β(s)=1) with a phase detector, a VCO (voltage controlled oscillator), and a loop filter in the feed-forward path, A(s). Figure 2 illustrates a phase lock loop as a feedback control system in block diagram form.
F
i
F
o
PHASE
DETECTOR
K
f
V
CO
K
o
s
Figure 2. Phase Lock Loop Block Diagram
The closed loop transfer function is:
Xo(s) Xi(s)
=
K
φ
K
o
s
F(s)
K
o
s
1 + K
φ
F(s)
where:
Kφ= the phase detector gain. Ko= the VCO gain. Since the VCO introduces a pole at the origin of the s-plane, Ko is divided
by s.
F(s) = the transfer function of the loop filter.
The 10E197 is designed to implement the phase detector and VCO functions in a unity feedback loop, while allowing the user to select the desired filter function.
Gain Constants
As mentioned, each of the three sections in the phase lock loop block diagram has an associated open loop gain constant. Further, the gain constant of the filter circuitry is composed of the product of three gain constants, one for each filter subsection. The open loop gain constant of the feed-forward path is given by
Kol = Kφ * Ko * K1 * Kl * K
d
eqt. 1
and obtained by performing a root locus analysis.
Phase Detector Gain Constant
The gain of the phase detector is a function of the operating mode and the data pattern. The 10E197 provides data
LOOP FILTER
F(s)
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separation for signals encoded in 2:7 or 1:7 RLL encoding schemes; hence, Tables 1 and 2 are coding tables for these schemes. Table 3 lists nominal phase detector gains for both 2:7 and 1:7 sync fields.
NRZ Data Sequence Code Sequence
00 1000 01 0100
100 001000 101 100100
111 000100 1100 00001000
1101 00100100
Table 1. 2:7 RLL Encoding Table
NRZ Data Sequence Code Sequence
00 X01 01 010
10 X00 1100 010001
1101 X00000 1110 X00001
1111 010000
An X in the leading bit of a code sequence is assigned the complement of the bit
Table 2. 1:7 RLL Encoding Table
Sync Pattern Read Mode Idle Mode
2:7 121 mV/radian 484 mV/radian 1:7 161 mV/radian 483 mV/radian
Table 3. Phase Detector Gain Constants
VCO Gain Constant
The gain of the VCO is a function of the tuning capacitor. For a value of 10pF a nominal value of the gain, Ko, is 20MHz per volt.
Filter Circuitry Gain Constant(s)
The open loop gain constant of the filter circuitry is given by:
Kfc = K1 * Kl * K
d
eqt. 2
The individual gain constants are defined in the appropriate subsections of this document.
Loop Filter
The two major functions of the loop filter are to remove any noise or high frequency components present in the phase detector output signal and, more importantly, to control the characteristics which determine the dynamic response of the phase lock loop; i.e. capture range, loop bandwidth, capture time, and transient response.
Although a variety of loop filter configurations exist, this section will only describe a filter capable of performing the signal processing as described in the Data Read Mode and the Idle Mode sections. The loop filter consists of a differential summing amplifier cascaded with an augmenting integrator which drives the VCOIN input to the 10E197 through a resistor divider network (Figure 3).
The transfer function and the element values for the loop filter are derived by dividing the filter into three cascaded subsections: filter input, augmenting integrator, and the voltage divider network (Figure 4).
Loop Filter Transfer Function
The open loop transfer function of the phase lock loop is the product of each individual filter subsection, as well as the phase detector and VCO. Thus, the open loop filter transfer function is:
Fo(s) = Kφ *
Fd(s) = Kd *
* F1(s) * Fl(s) * Fd(s)
K
o
s
F1(s) = K1 *
1
(s + p1)
*
1
[s2 + (2ζω ) s + ω2 ]
[s2 + (2ζω ) s + ω2 ]
where:
Fl(s) = Kl *
1 s
*
(s + z)
1
(s + p2)
o2o2
o1 o1
Figure 3. Loop Filter Circuitry
PUMPUP
PUMPDN
V
EEVCO
V
EEVCO
V
CCVCO
V
CCVCO
V
EEVCO
V
EEVCO
R
1
R
1
R
IA
R
A
C
A
R
V
R
O
D
B
C
O
R
3
R
1
R
1
C
IN
C
IN
V
O
MC34182
MC34182
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VOLTAGE
DIVIDER
FO(s)
AUGMENTNG INTEGRATOR
FI(s)
FILTER
INPUT
F1(s)
Fi(s)
F
(s)=F1
(s)Fi(s)Fd(s)
Figure 4. Loop Filter Block Diagram
A root locus analysis is performed on the open loop transfer function to determine the final pole-zero locations and the open loop gain constant for the phase lock loop. Note that the open loop gain constant impacts the crossover frequency and that a lower frequency crossover point means a much more efficient filter. Once these positions and constants are determined the component values may be calculated.
I
PUMPUP
I
PUMPDN
V
EEVCOVEEVCO
V
EEVCO
V
EEVCO
V
CCVCO
R
1
R
1
R
1
R
1
C
IN
V
01
MC34182
Figure 5. Filter Input Sunsection
Filter Input
The primary function of the filter input subsection is to convert the output of the phase detector into a single ended signal for subsequent processing by the integrator circuitry. This subsection consists of the 10E197 charge pump current sinks, two shunt capacitors, and a differential summing amplifier (Figure 5).
Hence, this portion of the filter circuit contributes a real pole and two complex poles to the overall loop transfer function F(s). Before these pole locations are selected, appropriate values for the current setting resistors (RSETUP and RSETDN) must be ascertained. The goal in choosing these resistor values is to maximize the gain of the filter input subsection while ensuring the charge pump output transistors operate in the active mode. The filter input gain is maximized for a charge pump current of 1.1mA; a value of 464 for both RSETUP and RSETDN yields a nominal charge pump current of 1.1mA.
It should be noted that a dual bandwidth implementation of the phase lock loop may be achieved by modifying the current setting resistors such that an electronic switch enables one of two resistor configurations. Figure 6 shows
a circuit configuration capable of providing this dual bandwidth function. Analysis of the filter input circuitry yields the transfer function:
F1(s) = K1 *
1
(s + p1)
*
1
where:
The gain constant is defined as:
K1 = A1 *
1
C
IN
eqt. 3
A1= op-amp gain constant for the
selected pole positions.
CIN = phase detector shunt capacitor.
[s2 + (2ζω ) s + ω2 ]
o1 o1
The real pole is a function of the input resistance to the op-amp and the shunt capacitors connected to the phase detector output. For stability the real pole must be placed beyond the unity gain frequency; hence, this pole is typically placed midway between the unity crossover and phase detector sampling frequency, which should be about ten times greater.
ELECTRONIC SWITCH
V
EEVCO
V
EEVCO
RSETUP
RSETDN
464
464
464
464
Figure 6. Dual Bandwidth Current
Source Implementation
The second order pole set arises from the two pole model for an op-amp. The open loop gain and the first open loop pole for the op-amp are obtained from the data sheets. Typically, op-amp manufacturers do not provide information on the location of the second open loop pole; however, it can be approximated by measuring the roll off of the op-amp in the open loop configuration. The second pole is located where the gain begins to decrease at a rate of 40dB per decade. The inclusion of both poles in the differential summing amplifier transfer function becomes important when closing the feedback path around the op-amp because the poles migrate; and this migration must be accounted for to accurately determine the phase lock loop transient performance.
Typically the op-amp poles can be approximated by a pole pair occurring as a complex conjugate pair making an angle of 45° to the real axis of the complex frequency plane. Two constraints on the selection of the op-amp pole pair are that
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the poles lie beyond the crossover frequency and they are positioned for near unity gain operation. Performing a root locus analysis on the op-amp open loop configuration and adhering to the two constraints yields the pole positions contributed by the op-amp.
Determination of Element Values
Since the difference amplifier is configured to operate as a differential summer the resistor values associated with the amplifier are of equal value. Further, the typical input resistance to the summing amplifier is 1k; thus, the op-amp resistors are set at 1 k. Having set the input resistance to the op-amp and selected the position of the real pole, the value of the shunt capacitors is determined using the following relationship:
p1 =
1
2πR1C
IN
eqt. 4
Augmenting Integrator
The augmenting integrator consists of an active filter with a lag-lead network in the feedback path (Figure 7).
V
IN
V
CCVCO
MC34182
R
IA
R
A
C
A
V
O2
R
IA
Figure 7. Integrator Subsection
Analysis of this portion of the filter circuit yields the transfer function:
F1(s) = Kl *
1 s
*
(s + z)
[s2 + (2ζω ) s + ω2 ]
o2o2
The gain constant is defined as:
where:
Al = op-amp gain constant for selected pole positions. RA = integrator feedback resistor. RlA = integrator input resistor.
Kl = Al *
R
A
R
lA
eqt. 5
The integrator circuit introduces a zero, a pole at the origin, and a second order pole set as described by the two pole model for an op-amp. As in the case of the differential summing amplifier, we assume the op-amp pole pair occur as
a complex conjugate pair making an angle of 45° to the real axis of the complex frequency plane; are positioned for near unity gain operation; and are located beyond the crossover frequency. Since both the summing and integrating op-amps are realized by the same type of op-amp (MC34182D), the open loop pole positions for both amplifiers will be the same.
Further, the loop transfer function contains two poles located at the origin, one introduced by the integrator and the other by the VCO; hence a zero is necessary to compensate for the phase shift produced by these poles and ensure loop stability. The op-amp will be stable if the crossover point occurs before the transfer function phase angle becomes 180°. The zero should be positioned much less than one decade before the unity gain frequency.
As in the case of the filter input circuitry, the poles and zero from this analysis will be used as open loop poles and a zero when performing the root locus analysis for the complete system.
Determination of Element Values
The location of the zero is used to determine the element values for the augmenting integrator. The value of the capacitor, CA, is selected to provide adequate charge storage when the loop is not sampling data. A value of 0.1µF is sufficient for most applications; this value may be increased when the RDCLK frequency is much lower than 4 MHz. The value of RA is governed by:
z =
1
2πRAC
A
eqt. 6
For unity gain operation of the integrating op-amp the value of RlA is selected such that:
RlA = RA eqt. 7
It should be noted that although the zero can be tuned by varying either RA or CA, caution must be exercised when adjusting the zero by varying CA because the integrator gain is also a function of CA. Further, the gain of the loop filter can be adjusted by changing the integrator input resistor RlA.
Voltage Divider
The input range to the VCOIN input is from 1.3V + VEE to
2.6V + VEE; hence, the output from the augmenting amplifier section must be attenuated to meet the VCOIN constraints. A simple voltage divider network provides the necessary attenuation (Figure 8).
V
IN
R
V
R
O
D
B
C
d
V
O
Figure 8. Voltage Divider Subsection
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In addition, a shunt filter capacitor connected between the VCOIN input pin and VEE provides the voltage divider subsection with a single time constant transfer function that adds a pole to the overall loop filter. The transfer function for the voltage divider network is:
Fd(s) = Kd *
1
(s + p2)
The gain constant, Kd, is defined as:
Kd =
1
Rv C
d
eqt. 9
The value of Kd is easily extracted by rearranging Equation 1:
Kd =
K
ol
Kφ * Ko * K1 * K
l
eqt. 10
The gain constant Kd is set such that the output from the integrator circuit is within the range 1.3V +VEE to 2.6V +VEE.
The pole for the voltage divider network should be positioned an octave beyond that for the filter input.
Determination of Element Values
Once the pole location and the gain constant Kd are established the resistor values for the voltage divider network are determined using the design guidelines mentioned above and from the following relationship:
K
d
2πp2
=
R
o
Ro + R
v
Having determined the resistor values, the filter capacitor is calculated by rearranging Equation 9:
Cd =
1
Rv K
d
eqt. 9a
Finally, a bias diode is included in the voltage divider network to provide temperature compensation. The finite resistance of this diode is neglected for these calculations.
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Calculations For a 2:7 Coding Scheme
Introduction
The circuit component values are calculated for a 2:7 coding scheme employing a data rate of 23Mbit/sec. Since the number of bits is doubled when the data is encoded, the data clock is at half the frequency of the RDCLK signal. Thus, the operating frequency for these calculations is 46MHz. Further, the pole and zero positions are a function of the data rate; hence, the component values derived by these calculations must be scaled if a different operating frequency is used. Finally, it should be noted that the values are optimized for settling time.
The analysis is divided into three parts: static pole positioning, dynamic pole positioning, and dynamic zero positioning. Dynamic poles and zeros are those which the designer may position, to yield the desired dynamic response, through the judicious choice of element values. Static poles are not directly controlled by the choice of component values.
Static Poles
Each op-amp introduces a pair of “static” complex conjugate poles which must lie beyond the crossover frequency. As obtained from the data sheets and laboratory measurements, the two open loop poles for the MC34182D are:
P*1a = – 0.1Hz
P*1b = –11.2Hz
Performing a root locus analysis and following the two guidelines previously stated, an acceptable pole set is:
P1a = – 5.65 + j5.65MHz P1b = – 5.65 – j5.65MHz
Both op-amps introduce a set of static complex conjugate poles at these positions for a total of four poles. Further, the loop gain for each op-amp associated with these pole positions is determined from the root locus analysis to be:
A1 = A2 = 2.48 e15
V V
In addition to the op-amps, the integrator and the VCO each contribute a static pole at the origin. Thus, there are a total of six static poles.
Dynamic Poles
The filter input and the voltage divider sections each contribute a dynamic pole. As stated previously , the filter input pole should be positioned midway between the unity crossover point and the phase detector sampling frequency. Hence, the open loop filter input pole position is selected as:
P*1 = –1.24MHz
The voltage divider pole is set approximately one octave higher than the filter input pole. Thus the open loop voltage divider pole position is picked to be:
P*2 = – 2.57MHz
Dynamic Zero
Finally, the zero is positioned much less than one decade before the crossover frequency; for this design the zero is placed at:
z = – 311Hz
Once the dynamic pole and zero positions have been determined, the phase margin is determined using a Bode plot; if the phase margin is not sufficient, the dynamic poles may be moved to improve the phase margin. Finally, a root locus analysis is performed to obtain the optimum closed loop pole positions for the dynamic characteristics of interest.
Component Values
Having determined the closed loop pole and zero positions the component values are calculated. From the root locus analysis the dynamic pole and zero positions are:
P1 = – 573kHz
P2 = – 3.06MHz
z = – 311Hz
Filter Input Subsection
Rearranging Equation 4:
CIN =
1
2π R1 p1
and substituting 573 kHz for the pole position and 1 k for the resistor value yields:
CIN = 278 pF
Augmenting Integrator Subsection
Rearranging Equation 6:
RA =
1
2
π  z
C
A and substituting 31 1Hz for the zero position and 0.1µF for the capacitor value yields:
RA = 5.11k
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From Equation 7 the value for the other resistors associated with the integrator op-amp are set equal to RA:
RlA = RA = 5.11k
Voltage Divider Subsection
The element values for the voltage divider network are calculated using the relationships presented in Equations 8, 9, and 10 with the constraint that this divider network must produce a voltage that lies within the range 1.3V + VEE to 2.6V + VEE. Restating Equation 9,
Kd =
K
ol
Kφ * Ko * K1 * K
l
From the root locus analysis Kol is determined to be:
Kol = 1.585 e51
V
mA sec
3
From Equation 3
K1 = A1 *
1
C
IN
and the gain constant K1 is:
K1 = 8.90 e21
V
mA sec
From Equation 5
Kl = Al *
R
A
R
lA
and the gain constant Kl is:
Kl = 2.48 e15
V V
Having determined the gain constant Kd , the value of Rv, is selected such that the constraints Rv > Ro and:
K
d
2πp2
=
R
o
Ro + R
v
are fulfilled. The pole position P2 is determined from the root locus analysis to be:
P2 = – 3.06MHz
Hence, Rv is selected to be:
Rv = 2.15k
and Ro is calculated to be:
Ro = 700
Finally, using Equation 8a:
Cd =
1
Rv K
d
eqt. 8a
the capacitor value, Cd is:
Cd = 98pF
Note that the voltage divider section can be used to set the gain, but the designer is cautioned to be sure the input value to VCOIN is within the correct range.
Component Scaling
As mentioned, these design equations were developed for a data rate of 23 Mbit/sec. If the data rate is different from the nominal design value the reactive elements must be scaled accordingly. The following equations are provided to facilitate scaling and were derived with the assumptions that a 2:7 coding scheme is used and that the RDCLK signal is twice the frequency of the data clock.
CIN = 278 *
46
f
eqt. 11
(pF)
46
f
Cd = 98 * eqt. 12(pF)
where f is the RDCLK frequency in MHz.
Example for an 11 Mbit/sec Data Rate
As an example of scaling, assume the given filter and a 2:7 code are used but the data rate is 11Mbit/sec. The dynamic pole positions, and therefore the bandwidth of the loop filter, are a function of the data rate. Thus a slower data rate will force the dynamic poles and the bandwidth to move to a lower frequency. From Equation 11 the value of CIN is:
CIN = 581pF
and from Equation 12 the value of Cd is:
Cd = 205pF Thus the element values for the filter are: Filter Input Subsection:
CIN = 581pF
R1 = 1k Integrator Subsection:
CA = 0.1µF
RA = 5.11k
RlA = 5.11k
Voltage Divider Subsection:
Cd = 205pF
Rv = 2.15k Ro = 700k
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2–12
Note, the poles P1 and P2 are now located at:
P1 = – 274kHz P2 = –1.47MHz
And, the open loop filter unity crossover point is at 300kHz. The gain can be adjusted by changing the value of RlA and the value of Cd. Varying the gain by changing Cd is not recommended because this will also move the poles, hence affect the dynamic 2 performance of the filter.
Calculations For a 1:7 Coding Scheme
Introduction
The circuit component values are calculated for a 1:7 coding scheme employing a data rate of 20Mbit/sec. Since the number of bits increases from two to three when the data is encoded, the data clock is at two-thirds the frequency of the RDCLK signal. Thus, the operating frequency for these calculations is 30MHz. As in the case of the 2:7 coding scheme the pole and zero positions are a function of the data rate, hence the component values derived by these calculations must be scaled if a different operating frequency is used.
Again, the analysis is divided into three parts: static pole positioning, dynamic pole positioning, and dynamic zero positioning.
Static Poles
As in the 2:7 coding example, an MC34182D op-amp is employed, hence the pole set is:
P1a = – 5.65 + j5.65MHz P1b = – 5.65
j5.65MHz
and the open loop gain is:
Al = A2 = 2.48 e15
V V
Since the op-amps introduce a set of complex conjugate poles, a total of four poles are introduced by the op-amp. In addition, the integrator and the VCO each contribute a pole at the origin for a total of six static poles.
Dynamic Poles
The filter input and the voltage divider sections each contribute a dynamic pole. As stated previously , the filter input pole should be positioned midway between the unity crossover point and the phase detector sampling frequency. Hence, the open loop filter input pole position is selected as:
P
*
1
= –1.1MHz
The voltage divider pole is set approximately one octave higher than the filter input pole. Thus, the open loop voltage divider pole position is selected as:
P
*
2
= – 2.28MHz
Dynamic Zero
Finally, the zero is positioned much less than one decade before the crossover frequency; for this design the zero is placed at:
z = – 311Hz
Once the dynamic pole and zero positions have been determined, the phase margin is determined using a Bode plot; if the phase margin is not sufficient, the dynamic poles may be moved to improve the phase margin. Finally, a root locus analysis is performed to obtain the optimum closed loop pole positions for the dynamic characteristics of interest.
Component Values
Having determined the closed loop pole and zero positions the component values are calculated. From the root locus analysis the dynamic pole and zero positions are:
P1 = – 541kHz P2 = – 2.73MHz
z = – 311Hz
Filter Input Subsection
Rearranging Equation 4
CIN =
1
2π R1 p1
and substituting 541kHz for the pole position and 1.0k for the resistor value yields:
CIN = 294 pF
Augmenting Integrator Subsection
Rearranging Equation 6
RA =
1
2π zC
A
and substituting 31 1Hz for the zero position and 0.1µF for the capacitor value yields:
RA = 5.11k
From Equation 7 the value for the other resistors associated with the integrator op-amp are set equal to RA:
RlA = RA = 5.11k
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Voltage Divider Subsection
The element values for the voltage divider network are calculated using the relationships presented in Equations 8, 9, and 10 with the constraint that this divider network must produce a voltage that lies within the range 1.3V + VEE to 2.6V + VEE. Restating Equation 9,
Kd =
K
ol
Kφ * Ko * K1 * K
l
From the root locus analysis Kol is determined to be:
Kol = 1.258 e51
V
MA
SEC
3
From Equation 3:
K1 = A1 *
1
C
IN
and the gain constant K1:
K1 = 8.42 e21
V
mA sec
From Equation 5:
Kl = Al *
R
A
R
lA
and the gain constant Kl is:
Kl = 2.48 e15
V V
Kd = 2.98 e6 sec
–1
Having determined the gain constant Kd , the value of Rv, is selected such that the constraints Rv > Ro and:
K
d
2πp2
=
R
o
Ro + R
v
are fulfilled. The pole position P2 is determined from the root locus analysis to be:
P2 = – 2.73MHz
Hence, Rv is selected to be:
Rv = 2.15k
and Ro is calculated to be:
Ro = 453
Finally, using Equation 8a:
Cd =
1
Rv K
d
eqt. 8a
the capacitor value, Cd is calculated to be:
Cd = 156pF
Again, note the voltage divider section can be used to set the gain, but the designer is cautioned to be sure the input value to VCOIN is within the correct range.
Component Scaling
As mentioned, these design equations were developed for a data rate of 20Mbit/sec. If the data rate is different from the nominal design value the reactive elements must be scaled accordingly. The following equations provided are to facilitate scaling and were derived with the assumptions that a 1:7 coding scheme is used and that the RDCLK signal is twice the frequency of the data clock:
CIN = 294 *
30
f
eqt. 13(pF)
30
f
Cd = 156 * eqt. 14(pF)
where f is the RDCLK frequency in MHz.
Example for an 10 Mbit/sec Data Rate
As an example of scaling, assume the given filter and a 1:7 code are used but the data rate is 10Mbit/sec. The dynamic pole positions and, therefore, the bandwidth of the loop filter, are a function of the data rate. Thus, a slower data rate will force the dynamic poles and the bandwidth to move to a lower frequency. From Equation 13 the value of CIN is:
CIN = 588pF
and from Equation 14 the value of Cd is:
Cd = 312pF Thus, the element values for the filter are: Filter Input Subsection:
CIN = 588pF
R1 = 1.0k
Integrator Subsection:
CA = 0.1µF
RA = 5.11k
RlA = 5.11k
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Voltage Divider Subsection:
Cd = 312pF Rv = 2.15k Ro = 453k
Note, the poles P1 and P2 are now located at:
P1 = – 271kHz
P2 = –1.36MHz And, the open loop filter unity crossover point is at 300kHz.
As in the case of the 2:7 coding scheme, the gain can be adjusted by changing the value of RlA and the value of Cd. Varying the gain by changing Cd is not recommended because this will also move the poles, hence affect the dynamic performance of the filter.
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OUTLINE DIMENSIONS
FN SUFFIX
PLASTIC PLCC PACKAGE
CASE 776–02
ISSUE D
0.007 (0.180) T L
–M
SNSM
0.007 (0.180) T L
–M
SNSM
0.007 (0.180) T L
–M
SNSM
0.010 (0.250) T L
–M
SNSS
0.007 (0.180) T L
–M
SNSM
0.010 (0.250) T L
–M
SNSS
0.007 (0.180) T L
–M
SNSM
0.007 (0.180) T L
–M
SNSM
0.004 (0.100)
SEATING PLANE
-T-
12.32
12.32
4.20
2.29
0.33
0.66
0.51
0.64
11.43
11.43
1.07
1.07
1.07 — 2
°
10.42
1.02
12.57
12.57
4.57
2.79
0.48
0.81 — —
11.58
11.58
1.21
1.21
1.42
0.50
10
°
10.92 —
1.27 BSC
A B C E F G H J K R U V W X Y
Z G1 K1
MIN MINMAX MAX
INCHES MILLIMETERS
DIM
NOTES:
1. DATUMS -L-, -M-, AND -N- DETERMINED WHERE TOP OF LEAD SHOULDER EXITS PLASTIC BODY AT MOLD PARTING LINE.
2. DIM G1, TRUE POSITION TO BE MEASURED AT DATUM -T-, SEATING PLANE.
3. DIM R AND U DO NOT INCLUDE MOLD FLASH. ALLOWABLE MOLD FLASH IS 0.010 (0.250) PER SIDE.
4. DIMENSIONING AND TOLERANCING PER ANSI Y14.5M, 1982.
5. CONTROLLING DIMENSION: INCH.
6. THE PACKAGE TOP MAY BE SMALLER THAN THE PACKAGE BOTTOM BY UP TO 0.012 (0.300). DIMENSIONS R AND U ARE DETERMINED AT THE OUTERMOST EXTREMES OF THE PLASTIC BODY EXCLUSIVE OF MOLD FLASH, TIE BAR BURRS, GATE BURRS AND INTERLEAD FLASH, BUT INCLUDING ANY MISMATCH BETWEEN THE TOP AND BOTTOM OF THE PLASTIC BODY.
7. DIMENSION H DOES NOT INCLUDE DAMBAR PROTRUSION OR INTRUSION. THE DAMBAR PROTRUSION(S) SHALL NOT CAUSE THE H DIMENSION TO BE GREATER THAN 0.037 (0.940). THE DAMBAR INTRUSION(S) SHALL NOT CAUSE THE H DIMENSION TO BE SMALLER THAN 0.025 (0.635).
VIEW S
B
U
Z
G1
X
VIEW D-D
H
K
F
VIEW S
G
C
Z
A
R
E
J
0.485
0.485
0.165
0.090
0.013
0.026
0.020
0.025
0.450
0.450
0.042
0.042
0.042 — 2
°
0.410
0.040
0.495
0.495
0.180
0.110
0.019
0.032 — —
0.456
0.456
0.048
0.048
0.056
0.020
10
°
0.430 —
0.050 BSC
-N-
Y BRK
D
D
W
-M-
-L-
28 1
V
G1
K1
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