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TYPICAL WPT DATA ENTRY DISPLAYS
WAYPOINT PARAMETER SELECTED/DATA
I
/
KNED IN SCRATCH PAD, LAT, LONG,
ALT, RNG, BRG, SET, MAPLINE,
--J MAP OFST. TOT LNG. OR CMD CRS
------+-------i
OPTION KEY PRESSED.
*ONLY THE RESPECTIVE CHARACTER
LEGENDS (S. -, W, N. +, E, OR BLANK)
APPLICABLE TO THE PARAMETER
SELECTED WILL APPEAR ON THE
OPTION DISPLAY LEGEND
-
Figure 22-13. DEU ReconnaissanceS election
22-21 ORIGINAL
NAVAIR Ol-F14AAD-1
22.5.2 In-Flight Entry of Reconnaissance Waypoint
Parameters. The RIO may update the waypoint
tile at any time when a reconnaissances teering
mode is engaged,w ithout affecting the Currents teering.
In order for the pilot to use the updated reconnaissance
parameters,h e must reselectt he steeringm ode.
22.5.3 One-Fix Update. Unless the aircraft is flying
in a ITIDS net, it is recommended that one-fix position
update be performed just prior to flying over the intended
target to minimize miss distance. Refer to Chapter
20 for the procedures for one-fix position updates.
22.5.4 Plotting Command Course/Map Target
Leg. This optional procedure provides the flightcmw
with additional steering cue/information on the HSD. If
a tile waypoint is available, the RIO may use this waypoint
to mark the end of a target leg by performing the
following steps:
1. On the DEU, select WPT and enter the designated
waypoint for reconnaissance.
2. Select RNG and enter the target length of the reconnoitered
target.
3. Select BRG and enter the command course of the
reconnoitered target.
4. Press SET and enter the number of the available
(or free) waypoint.
5. Select MENU.
6. Select PLOT.
7. Select DRAW. The DEU will respond “Plot
from . . .” Enter waypoint number to which aircraft
is flying. When DEU responds “‘Plot to. . .,”
enter the waypoint number used in step 4.
22.5.5 Cycling Sensors. The RIO will put the
FILM switch on the CPS in the RUN position when the
RANGE-TO-GO goes to zero or transitions to RANGE
REMAINING. The RIO will turn off the selected sensors
when RANGE REMAININ G goes to zero.
22.6 PILOT RECONNAISSANCE OPERATION
A sensor operating button is provided on the pilot
control stick. With the SYSTEM switch on the controller
processor signal unit set to RDY and any or all sensor
selector switches in the ready position, the activated
sensor can be cycled by the pilot pressing the BOMB
button on the control stick. This is the only TARPS
control capability provided to the pilot. Each camera
will cycle at its proper rate for velocity/height ratio
(V/H) and the IRLS will ruu continuously at the proper
speed until the pilot releases the BOMB button.
Note
The BOMB button will not initiate camera
operation with the expanded chaff adapter
installed.
22.6.1 Navigation Visual Surface Waypolnt
Update. Unless the aircraft is flying in a JTIDS net, it
is recommended that the one-fix position update be performed
just prior to flying over the intended target to
minimizemiss distance. Refer to one-fixpositionupdate
in Chapter 20 for INS update operations.
22.6.2 Pilot TARPS Steering. TARPS aircraft
steering is displayed on the MI and on the HUD in A/G
and A/A (weapon not selected). The VDI is selected via
the MPD RECON DATA status format.
HUD TARPS steering using TARPS symbology
(Figure 22-9) is obtained by selecting a reconnaissance
steering mode (FTP, CCRS, or MAP) on the recomtaissance
MFD RECON DATA status format.
Note
In addition to the steering cues, the
reconnaissance target designator will be
positioned on the HUDNDI to indicate
actual target position. (It is recommended to
perform a surface waypoint update to the
navigation.system to ensure that the
reconnaissance target designator will
overlay the expected target site.) Steering is
accomplished by noting the direction that the
recommissances teering symbol is displaced
from the velocity vector. Banking the aircraft
in the same direction to achieve and maintain
alignment of the two symbols will produce
the desired flightpath. If in PTP steering,
match aircraft heading with reconnaissance
command heading marker.
At the completion of a PTP, CCRS, or MAP mission,
the TARPS symbology will be removed from the
HUD/VDI. In addition, the steering mode will become
unboxedontheMFDREcoNDATAstatus format Them
is no sequencingo f waypoints.T o steert o the next waypoin&
the d&i waypint number must be selected.
ORIGINAL 22.22
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F-14D 飞行手册 Flight Manual 3(49)
