Intel 820E Benutzerhandbuch

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Intel
®
 820E Chipset 
R
 
 
 
Design Guide 
 
151 
Figure 76. Test Load vs. Actual System Load 
V
TT
Q
Q
SET
CLR
D
Vcc
CLK
R
TEST
Test load
Driver pin
Driver pad
T
REF
T
CO
I/O Buffer
Q
Q
SET
CLR
D
Vcc
CLK
Driver pad
T
FLIGHTSYSTEM
I/O Buffer
V
TT
R
TT
Actual system load
Receiver pin
test_actual_load
 
The previous figure shows the different configurations for T
CO
 testing and flight time simulation. The 
flip-flop represents the logic input and driver stage of a typical AGTL+ I/O buffer. T
CO
 timings are 
specified at the driver pin output. T
FLIGHT-SYSTEM
 usually is reported by a simulation tool as the time from 
the driver pad starting its transition to the time when the receiver’s input pin sees a valid data input. Since 
both timing numbers (T
CO
, T
FLIGHT-SYSTEM
) include propagation time from the pad to the pin, it is 
necessary to subtract this time (T
REF
) from the reported flight time to avoid double counting. T
REF
 is 
defined as the time required for the driver output pin to reach the measurement voltage, V
REF
, starting 
from the beginning of the driver transition at the pad. T
REF
 must be generated using the same test load for 
T
CO
. Intel provides this timing value in the AGTL+ I/O buffer models. 
In this manner, the following valid delay equation is satisfied: 
Equation 8. Valid Delay Equation 
Valid delay = T
CO
 + T
FLIGHT-SYS
 – T
REF
 = T
CO-MEASURED
 + T
FLIGHT-MEASURED 
This valid delay equation yields the total time from when the driver sees a valid clock pulse to the time 
when the receiver sees a valid data input. 
3.2.6.3. 
Flight Time Hardware Validation 
When a measurement is made in the actual system, T
CO
 and flight time do not need T
REF
 correction since 
these are the actual numbers. These measurements include all of the effects pertaining to the 
driver-system interface, and the same is true for T
CO
. Therefore, the sum of the measured T
CO
 and the 
measured flight time must be equal the valid delay calculated previously.