Technical data

Product Specification
HIF-2121/R5 CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 965-1176-601 REV: D SHEET 53
6.2.2 Mode 2 -- Excessive Terrain Closure Rate
Mode 2 provides two types of alerts based on aircraft gear/flap configuration, radio altitude (terrain clearance), and how
rapidly that radio altitude is decreasing (closure rate). Barometric altitude of the airplane is not important in initiating this
warning.
These two alerts are commonly referred to as Mode 2A, described in sections 6.2.2.1 and 6.2.2.2, and as Mode 2B, described
in section 6.2.2.3.
Differentiating and scaling radio altitude generates closure rate. As the closure rate term is inherently noisy, especially over
irregular terrain, extensive rate limiting and filtering must be used to obtain an accurate closure rate value for computation.
The computer uses a number of different sets of sophisticated rate limits and filter methods to allow maximum sensitivity
during cruise, while providing progressively less sensitivity during the landing phases of flight. These rate limits vary as a
function of gear and flap position, aircraft speed, and whether or not the aircraft is on an ILS approach. It is this rate limiting
and filtering that determines the effectivity of Mode 2 in providing advance alerts, while avoiding unwanted or nuisance
alerts.
Altitude rate is combined with closure rate in the filtering method to provide “lead” information. Increasing the altitude
descent rate will tend to speed up the alert occurrence. Reducing the altitude descent rate, or initiating a climb, will tend to
delay the alert occurrence, or reduce the time that the alert is on.
Figure 6.2.2-1 shows the block diagram for Mode 2 alerts.
CLOSURE RATE DETECTION
RADIO RATE
MODE 2
OUTPUT
5733 FPM
30 FT
CLOSURE RATE (THOUSAND FPM)
MODE 2 ENVELOPE
(FOR GA FAST, GA SLOW NOT SHOWN)
MODE 2B INHIBIT
ILS MODE 2B
FLAPS DOWN
9800 FPM
3545 FPM
1220 FT
1650 FT
@ LE 220 KTS
2450 FT
@ LE 310 KTS
2038 FPM
AIRSPEED
FLAPS DOWN
GEAR DOWN
TIME CONSTANT
RATE LIMITS
FILTER
FLAPS DOWN
GEAR DOWN
ALTITUDE (ASL)
MODE 2
AUDIO
MODE 2
VISUAL
MODE 2
ALTITUDE
GAIN
(RADIO ALT RATE)
X
Y
X
RADIO ALTITUDE
Y
MODE 2 TAKEOFF
FIGURE 6.2.2-1: MODE 2 BLOCK DIAGRAM
Radio altitude, indicating the vertical distance between the aircraft and the underlying terrain, is differentiated to determine
the rate of change in this vertical distance. Any decrease in this vertical distance indicates potential ground contact for the
aircraft. Decreasing radio altitude may be the result of reducing the aircraft’s altitude, an increase in height of the terrain, or a
combination of both effects.
The computed closure rate is applied to the appropriate alert envelope, where the closure rate value is compared against the
actual radio altitude value, to determine the alert conditions as described below.










