Honeywell SPZ-8000 - Glossary of Terms; Attitude Director Indicator (ADI) Command Cue

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
7-1
System Limits
7. System Limits
GLOSSARY OF TERMS
This glossary gives a brief description of the flight guidance computer
control laws. These terms are used throughout this section and the
Modes of Operation section. The performance and operating limits for
these items are defined in Table 7--1. The terms included in this glossary
are:
D Attitude director indicator (ADI) command cue
D Glideslope gain programming
D Glideslope capture (GS CAP)
D Glideslope track (GS TRACK)
D Lateral beam sensor (LBS)
D Localizer capture 1/2 (LOC CAP 1/2), back course capture 1/2 (BC
CAP 1/2)
D Localizer track 1/2 (LOC TRACK 1/2), back course track 1/2, (BC
TRACK1/2)
D T rue airspeed (TAS) gain programmer
D Vertical beam sensor (VBS)
D VOR capture (VOR CAP)
D VOR track
D VOR over station sensor (VOR OSS)
D VOR after over station sensor 1/2 (VOR AOSS 1/2).
Attitude Director Indicator (ADI) Command Cue
When a command signal is applied to the cue input, the cue moves left
or right (roll) and up or down (pitch). This displays the visual command
that the pilot follows to fly along the desired flight path. If the information
required to fly the desired flight path becomes invalid, the command cue
is removed from the display.