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ACT4489-F Datasheet(PDF) 2 Page - Aeroflex Circuit Technology

Part # ACT4489-F
Description  ACT 4489 SINGLE TRANSCEIVER FOR MIL-STD-1553/1760
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Manufacturer  AEROFLEX [Aeroflex Circuit Technology]
Direct Link  http://www.aeroflex.com
Logo AEROFLEX - Aeroflex Circuit Technology

ACT4489-F Datasheet(HTML) 2 Page - Aeroflex Circuit Technology

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Aeroflex Circuit Technology
SCD4489 Rev A 1/29/98 Plainview NY (516) 694-6700
2
for the removal of the transmitter
output from the line. A logic “1”
signal applied to the “INHIBIT” takes
priority over the condition of the
data
inputs
and
disables
the
transmitter (See Transmitter Logic
Waveform,
Figure 1).
The
Transmitter may be safely operated
for an indefinite period with the bus
(point A) short circuited at 100%
duty cycle.
Receiver:
The
Receiver
section
accepts
bi-phase differential data at the
input and produces two TTL signals
at the output. The outputs are DATA
and DATA, and represent positive
and negative excursions of the input
beyond a pre-determined threshold
(See Receiver Logic Waveform,
Figure 2).
The pre-set internal thresholds will
detect data bus signals, point A
Figure 5, exceeding 1.20 Volts P-P
and reject signals less than 0.6
Volts
P-P
when
used
with
a
transformer (See Figure 5 for
transformer
data
and
typical
connection).
A low level at the RX Strobe
input inhibits the DATA
and
DATA outputs. If unused, a 2K
pull-up
to
+5
Volts
is
recommended.
DATA IN
DATA IN
INHIBIT
LINE TO LINE
OUTPUT
Note: DATA and DATA inputs must be complementary waveforms or 50% duty cycle average, with no delays between them,
and must be in the same state during off times (both high or low).
Figure 1 — Transmitter Logic Waveforms Idealized
Figure 2 — Receiver Logic Waveforms Idealized (ACT4489)
Note overlap
LINE TO LINE
INPUT
DATA OUT
DATA OUT
STROBE


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