Garmin GIA 63W Installation Manual page 90

4.10.2 Automatic Flight Control System Outputs
Pin Name
ANALOG ROLL STEERING HI
ANALOG ROLL STEERING LO (GROUND)
Variable-amplitude output, which is proportional to the aircraft roll command from the GPS navigation
system.
Amplitude:
Load Impedance:
Scaling:
Range:
Resolution:
Accuracy:
Pin Name
HEADING DATUM HI
HEADING DATUM LO (GROUND)
Outputs heading datum information to AFCS.
Amplitude:
Load Impedance:
Scaling:
Range:
Resolution:
Accuracy:
Pin Name
COURSE DATUM HI
COURSE DATUM LO (GROUND)
Outputs course datum information to AFCS.
Amplitude:
Load Impedance:
Scaling:
Range:
Resolution:
Accuracy:
GIA 63/GIA 63W Installation Manual
190-00303-05
DC
-15 to +15 Vdc
> 5 kΩ
2.0 Vdc per degree of roll command
0 ± 7.5 degrees of roll
± 0.05° or better
± 0.3°
DC
-15 to +15 Vdc
> 5 kΩ
0.55 Vdc per degree of heading error
0 ± 27 degrees
± 0.15° or better
± 1°
DC
-15 to +15 Vdc
> 5 kΩ
0.21 Vdc per degree of course error
0 ± 71 degrees
± 0.15° or better
± 1°
Connector Pin
P606 34
P606 36
Connector Pin
P606 46
P606 47
Connector Pin
P606 48
P606 49
I/O
Out
--
I/O
Out
--
I/O
Out
--
Page 4-27
Revision S