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Figure. 23-2. DD NAV GRID Data Entry
23.1.2 NAV GRID Displays. NAV GRID can be
displayed independently on both the TSD and TlD in
either a ground-stabilized or aircraft-stabilized format.
23.1.2.1 Tactical Information Display. The l’lD
NAV GRID display is enabled by selecting the A/C
STAB position of the TlD mode switch. Selecting this
position directly from ATTK results in an aircraft-stabilized
NAV GRID. Own aimrat? is fixed at the bottom
center of the TID with the top of the display oriented to
own-aircraft magnetic heading (Figure 23.3, detail A).
A ground-stabilizedN AV GRID display on the TID
is achieved by moving the TID MODE switch to GND
STAB then to A/C STAB. Gwn aircraft is initially displayed
at the center of the TTD. The top of the TID is
oriented to magnetic north. Chvn-aircraft and sensor
tracks transit the display in the direction of magnetic
headinga t own-aircraft groundspeedw hile the grid and
any waypoint positions remain fixed (Figure 23.3,
detail B).
The grid itself is representedb y grid strobese manating
from grid origin. Grid center is oriented to grid
heading (threat axis) with each sector bounded by two
strobes.S hort tic marks on the strobesr epresent5 0-mile
increments t?om grid origin, longer tic marks represent
lOOmile increments. A maximum of seven range tics
(350 miles) is displayed. When the grid contains six
sectors, no range tics are displayed on the center strobe.
Selectable range scales are 25,50,100,200, and 400
in either stabilized mode. A TID offset can be utilized
to reposition own-aircratl anywhere on the display. The
grid is repositioned accordingly and may only be partially
displayed (Figure 23-3, details B and C). Offset
positioning is canceled by momentarily cycling out of
the selected STAB mode.
Tactical use of the NAV GRID often makes it desk
able to reference tracks, waypoints, or own-aircraft position
as a range and bearing from grid origin rather than
Tom own-aircraft. This is accomplished by RIO seleetion
ofNAV GFUD on the DD (SPL category) as shown
inFigure 23.2.
23.1.2.2 Tactical Situation Display. The TSD format
can be selected on any MFD. NAV GRID can be
selected for display via the GRID pushtile on the TSD
DCL format (Figure 23.4). Lie the TID, the TSD can
‘23-3 ORIGINAL
NAVAIR 01.F14AALb1
AIRCRAFT
STABlUZEO
NAVGRlO NOT
BOXED ON DO.
ORIGINAL
(AT)2-F50D-274-O
Figure 23-3. TlD NAV GRID Displays
23-4
NAVAIR 01.Fl4AAD1
Figure 234. TSD NAV GRID Display
display the NAV GRID in either ground- or aircraftstabilii
formats as selectedb y the GSTAB or ASTAB
pushtiles. The ASTAB display has own-aircraft position
fixed on the lower third of the display with the top of the
display rapresenting own-aircraft magnetic heading.
The GSTAB display initializes with own-aircraft at the
center of the display. The top of the display represents
magnetic north. Own-aimaft and sensor tracks transit
the display based on magnetic heading and groundspeed
while the grid and any waypoint positions remain fixed.
The grid itself is displayed as on the TlD, with up to
six sectors defined by strobes emanating &om grid origin
and centeredo n grid beading( threata xis). Short and
long tic marks represent SO- and 100~mile increments,
respectively. Any TSD range scale (25,50,100,200, or
400) is selectable.F uture softwarew ill include an OFFSET
and EXF’AND capability for all TSD formats. Unlike
the TKD, bearing and range data hooked tracks or
waypoints cannot be referenced to grid origin.
23-5 (Reverse Blank) ORIGINAL
NAVAIR Ol-Fl4IuP1
CHAPTER 24
LANTIRN Targeting System
Reserved.
241 (Reverse Blank). ORIGINAL
PART IX
Flightcrew Coordination
Chapter 37 - Flightmw Coordination
Chapter 38 - .%imaft Self-Test
91 (ReverseB lanhj ORIGINAL
NAVAIR 0%F14AAD-1
CHAPTER 37
Flightcrew Coordination
37.1 INTRODUCTION
The duties of the pilot/RIO team are necessarily integrated
and contribute to the performance of the other.
Successful crew interaction can provide cockpit synergy
that significantly improves mission success. However,
a pilot/RIO team that does not interact successfully can
be a major detriment to mission success,I n this chapter,
specific responsibilities are delineated for each phase of
flight. Specific mission flightcrew responsibilities are
also delineated.
37.2 PILOT AND RIO RESPONSIBILITIES
37.2.1 Aircrew Coordination. Aircrew coordination
is the flightcrew’s use and integration of all available
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