Honeywell SPZ-8000 - Apr 15;93

10J1B;1OJ2B
r
———— ——.
Az-slo
OADC
I
ASCB “A” OATA
(
I
ASCO “B” DATA
(
L——————.
r
——————.
IRS
I
ASCB “A OATA
(
I
ASCS %“ OATA
(
L
———. ——.
AUTOPILOT YAW AXIS
9J 1
—
11
12
—
—
14
15
—
13*
-v
Flight Director/Autopilot
Yaw Channel Mode Flow Diagram
Figure 261 (Sheet 1)
4==
1
2
—
1
2
—
.—— — ———. ———— ————
FZ-SmFLIGNTGUIDANCE COMPUTER
-—..
ASCB A
INTERFACE
1-
==1-
-r
I
I
ASCB ‘A
I I
e,
YAW RATE
I
(
TASIIAS
)
———— .——
TO SH 2
NOTES
—.
1
2
3
DATA FROM ASCB’’A’’ AND ‘0”1S
AVERAGED TOGETHER TO PROVIOE
THE sELECTED SIOE WITH THE
APPLICABLE OUTPUTS INDICATED IF
ONE OF THE SIGNALS IS INVALIO
AND AVERAGING IS NOT POSSIBLE
THEN THE SYSTEM SWITCHES TO
SINGLE SIOE OPERATION uSING
THE SIGNAL FROM THE VALID
SENSOR
THE SWITCH NOMENCLATURE
CAUSES THE SWITCH TO CHANGE
FROM STATE SHOWN
POLARITY SIGNS AT SUMMATION
POINTS DENOTE SIGNAL
RELATIoNSHIPS
NOTE 1
-— ——— — . — — — . — — — —— —— — — —— —
AO.13665 I .R2
22-14-00
Page 298.145/298.146
Apr 15/93
Use or disclosure of information on this page is subject to the restrictions on the title page of this document,