12
11. The relationship between Full Width Half Maximum and RMS
values for Spectral Width is derived from the assumption of a
Gaussian shaped spectrum which results in a 2.35 X RMS = FWHM
relationship.
12. The optical rise and fall times are measured from 10% to 90%
when the transmitter is driven by a 25 MBd (12.5 MHz square-
wave) input signal. The ANSI T1E1.2 committee has designated
the possibility of defining an eye pattern mask for the transmitter
optical output as an item for further study. Avago Technologies
will incorporate this requirement into the specifications for these
products if it is defined. The HFBR-59XXL products typically
comply with the template requirements of CCITT (now ITU-T) G.957
Section 3.2.5, Figure 5 for the STM- 1 rate, excluding the optical
receiver filter normally associated with single mode fiber
measurements which is the likely source for the ANSI T1E1.2
committee to follow in this matter.
13a. Systematic Jitter contributed by the transmitter is defined as the
combination of Duty Cycle Distortion and Data Dependent Jitter.
Systematic Jitter is measured at 50% threshold using a 155.52
MBd (77.5 MHz square-wave), 223-1 pseudorandom data pattern
input signal.
13b. Duty Cycle Distortion contributed by the transmitter is measured
at the 50% threshold of the optical output signal using an IDLE
Line State, 125 MBd (62.5 MHz square-wave), input signal.
13c. Data Dependent Jitter contributed by the transmitter is specified
with the FDDI test pattern described in FDDI PMD Annex A.5.
14a. Random Jitter contributed by the transmitter is specified with a
155.52 MBd (77.5 MHz square-wave) input signal.
14b.Random Jitter contributed by the transmitter is specified with an
IDLE Line State, 125 MBd (62.5 MHz square-wave), input signal.
See Application Information - Transceiver Jitter Performance
Section of this data sheet for further details.
15a. This specification is intended to indicate the performance of the
receiver section of the transceiver when Input Optical Power signal
characteristics are present per the following definitions. The Input
Optical Power dynamic range from the minimum level (with a
window time-width) to the maximum level is the range over which
the receiver is guaranteed to provide output data with a Bit Error
Rate (BER) better than or equal to 1 x 10-10.
At the Beginning of Life (BOL) over the specified operating
temperature and voltage ranges 23 input is a 155.52 MBd, 2 - 1
PRBS data pattern with 72 “1” s and 72 “0”s inserted per the
CCITT (now ITU-T) recommendation G.958 Appendix I.
Receiver data window time-width is 1.23 ns or greater for the
clock recovery circuit to operate in. The actual test data window
time-width is set to simulate the effect of worst case optical input
jitter based on the transmitter jitter values from the specification
tables. The test window time-width is HFBR-5961L 3.32 ns.
Transmitter operating with a 155.52 MBd, 77.5 MHz square-wave,
input signal to simulate any cross-talk present between the
transmitter and receiver sections of the transceiver.
15b.This specification is intended to indicate the performance of the
receiver section of the transceiver when Input Optical Power signal
characteristics are present per the following definitions. The Input
Optical Power dynamic range from the minimum level (with a
window time-width) to the maximum level is the range over which
the receiver is guaranteed to provide output data with a Bit Error
Rate (BER) better than or equal to 2.5 x 10-10.
• At the Beginning of Life (BOL)
• Over the specified operating temperature and voltage ranges
• Input symbol pattern is the FDDI test pattern defined in FDDI
PMD Annex A.5 with 4B/5B NRZI encoded data that contains a
duty cycle base-line wander effect of 50 kHz. This sequence
causes a near worst case condition for inter-symbol interference.
• Receiver data window time-width is 2.13 ns or greater and
centered at mid-symbol. This worst case window time-width is
the minimum allowed eye-opening presented to the FDDI PHY
PM_Data indication input (PHY input) per the example in FDDI
PMD Annex E. This minimum window time-width of 2.13 ns is
based upon the worst case FDDI PMD Active Input Interface
optical conditions for peak-to-peak DCD (1.0 ns), DDJ (1.2 ns)
and RJ (0.76 ns) presented to the receiver.
To test a receiver with the worst case FDDI PMD Active Input jitter
condition requires exacting control over DCD, DDJ and RJ jitter
components that is difficult to implement with production test
equipment. The receiver can be equivalently tested to the worst
case FDDI PMD input jitter conditions and meet the minimum
output data window time-width of 2.13 ns. This is accomplished
by using a nearly ideal input optical signal (no DCD, insignificant
DDJ and RJ) and measuring for a wider window time-width of 4.6
ns. This is possible due to the cumulative effect of jitter
components through their superposition (DCD and DDJ are directly
additive and RJ components are rms additive). Specifically, when
a nearly ideal input optical test signal is used and the maximum
receiver peak-to-peak jitter contributions of DCD (0.4 ns), DDJ (1.0
ns), and RJ (2.14 ns) exist, the minimum window time-width
becomes 8.0 ns -0.4 ns - 1.0 ns - 2.14 ns = 4.46 ns, or conservatively
4.6 ns. This wider window time-width of 4.6 ns guarantees the
FDDI PMD Annex E minimum window time-width of 2.13 ns under
worst case input jitter conditions to the Avago Technologies
receiver.
• Transmitter operating with an IDLE Line State pattern, 125 MBd
(62.5 MHz square-wave), input signal to simulate any cross-talk
present between the transmitter and receiver sections of the
transceiver.
16a. All conditions of Note 15a apply except that the measurement is
made at the center of the symbol with no window time- width.
16b.All conditions of Note 15b apply except that the measurement is
made at the center of the symbol with no window time-width.
17a. Systematic Jitter contributed by the receiver is defined as the
combination of Duty Cycle Distortion and Data Dependent Jitter.
Systematic Jitter is measured at 50% threshold using a 155.52
MBd (77.5 MHz square- wave), 223 - 1 psuedorandom data pattern
input signal.
17b. Duty Cycle Distortion contributed by the receiver is measured at
the 50% threshold of the electrical output signal using an IDLE
Line State, 125 MBd (62.5 MHz square-wave), input signal. The
input optical power level is -20 dBm average.
17c. Data Dependent Jitter contributed by the receiver is specified
with the FDDI DDJ test pattern described in the FDDI PMD Annex
A.5. The input optical power level is -20 dBm average.
18a. Random Jitter contributed by the receiver is specified with a
155.52 MBd (77.5 MHz square- wave) input signal.
18b.Random Jitter contributed by the receiver is specified with an
IDLE Line State, 125 MBd (62.5 MHz square-wave), input signal.
The input optical power level is at maximum “PIN Min. (W)”. See
Application Information - Transceiver Jitter Section for further
information.
19. This value is measured during the transition from low to high
levels of input optical power.
20. This value is measured during the transition from high to low
levels of input optical power. At Signal Detect Deassert, the
receiver outputs Data Out and Data Out Bar go to steady PECL
levels High and Low respectively.
21. The Signal Detect output shall be asserted within 100 us after a
step increase of the Input Optical Power.
22. Signal detect output shall be de-asserted within 350 µs after a
step decrease in the Input Optical Power. At Signal Detect
Deassert, the receiver outputs Data Out and Data Out Bar go to
steady PECL levels High and Low respectively.
23. The HFBR-5961L transceiver complies with the requirements for
the trade-offs between center wavelength, spectral width, and
rise/fall times shown in Figure 7. This figure is derived from the
FDDI PMD standard (ISO/IEC 9314-3 : 1990 and ANSI X3.166 - 1990)
per the description in ANSI T1E1.2 Revision 3. The interpretation
of this figure is that values of Center Wavelength and Spectral
Width must lie along the appropriate Optical Rise/Fall Time curve.