Honeywell SPZ-8000 - Page 581

-——— ——— --—— ——
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FZ-SZOPLIGNTGUIDANCE COMPUTER
17&ooTuRNPITcHc0N7R0LLER
1 w
——— ———
10.ll B/10J2B
I
1
2
—
i7
;8
;5
%
50
1
2
IC4
10
—
— -15vDC EXC
— +15vDC EXC
~
AVERAGED
>
TURN KNOB OUTPUT
TO SH4
TKOO
I
I
I
I
L—
I
‘f=ilil
60
I
II
57
I
RIGHT ROLL
12
5s
I
13
55
L
.— J
14 56
●
———
A
1
r
——— ———
AZ-810
DADC
I
=-”
=
ASC8 A
INTERFACE
-v
I
L
“cB’’BMTAm
——— ———
NOTES
1.l’HEFOLLOWING ASCB “A AND “W DATA (SH1
THRU 4) IS AVERAGED IN THE FZ-820
● ROLL ATTITUDE
● ROLL RATE
TO SH 1
r
———
IRS
I
I
I
———
(
ASCB “K DATA ‘4
15
ASCB “W
DATA
(
12
13
V65J 10
I 1 I
I
TO SH4
. TAS
● LATERAL ACCEL
THE FOLLOWING ASCB “A OR “’W DATA (SH1
THRU 4) IS PROVIDED FROM THE COUPLED SIDE
● HEADING ERROR
● COURSE ERROR
(NOTE 1)
● HEADING
● LATERAL STEERING CMO
● DME
. ALTITuDE
● RADIO OEVIATION
IF ONE OF THE SIGNALS IS INVALIO AND AVERAG.
ING IS NOT POSSIBLE. THEN THE SYSTEM
SWITCHES TO SINGLE SIDE OPERATION USING
THE SIGNAL FROM THE VALID SENSOR.
2 THE SWITCH NOMENCLATURE CAUSES THE
SWITCH TO CHANGE FROM STATE SHOWN
P=sY=OL=N~TZ – 65J
I
T
(
ASCG “< OATA 16
17
I
ASCB “W DATA
(
1
NOTE 1
ASCB w
●
INTERFACE
ROLL ATTITUOE
I
3. POLARITY SIGNS AT SUMMATION POINTS
DENOTE SIGNAL RELATIONSHIPS
HEADING ERROR
IGP-820FLIGHT
llJ1
GUIDANCE CONTROLLER
10J1J
I %“
r
(H) ~
9
11
SYNC -
TACH
(L) z,
HDG
SEL
KNOB
Plso
: ;
~
—
}
HDG
HDGt40LDERRoR
TO (SH.11
SELECTED
TO ASCO
—
INTERFACE
(H)
)
HoG SYNC
(c)
k————— —A
——— ——— —.. — ——— ——— ——— ——— ——— ——— ——
AD 13663 @ R4
HDG SELECT AND HDG HOLO MODES
F1ight Director/Autopilot
Roll Channel Mode Flow Diagram
Figure 259 (Sheet 1)
22-14-00
Page 298.101/298.102
Aug 15/91
Use or dwclosure of mformallon on Ihls page KSsub]ect 10 the restrlcllons on the title page of this document