Honeywell PRIMUS 1000 - Localizer Mode Tracking Profile View; Localizer Tracking Display

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Modes of Operation
8-16
When the system acquires thelocalizer captureconditions, thecourse
error signal is removed from the lateral calculations. This leaves
localizer gain programming to track the localizer signal, as shown in
figure 8--13, and to compensate for localizer beam standoff in the
presence of a crosswind. The system automatically compensates for
a crosswind of up to 45_ course error. Figure 8--14 shows the PFD in
the localizer tracking mode.
Localizer Mode Tracking Profile View
Figure 8--13
2020
2020
3030
3030
60
IN
40
AD--50983--R1@
Localizer Tracking Display
Figure 8--14