Localizer Mode Capture Plan View - Honeywell PRIMUS 1000 Pilot's Manual

Integrated avionics system for embraer 145
Hide thumbs Also See for PRIMUS 1000:
Table of Contents

Advertisement

PRIMUSr1000 Integrated Avionics System
NOTES:
1. When flying a localizer intercept, the optimum
2. The pilot should not intercept the localizer at angles
When the course select pointer is set on the coupled side HSI using the
CRS knob on the GC, the course select error signal is established. This
signal represents the difference between actual aircraft heading and
the selected aircraft course.
The course error signal is routed from the IAC' s SG to the IAC' s flight
control function.
The radio deviation signal is routed from the navigation receiver to the
electronic flight instrument system (EFIS), and then to the flight control
function where the signal is lateral gain programmed.
Modes of Operation
8-14

Localizer Mode Capture Plan View

Figure 8--11
intercept angle is 45_ .
greater than 90_ . At angles greater than 90_ , the
system automatically captures the back course.
A28--1146--112--00

Hide quick links:

Advertisement

Table of Contents
loading

Table of Contents