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between adjacent map legs). The altitude entered is the
target MSL altitude. The target length is entered via the
DEU. Figure 22-13 shows TARPS DEU entry matrix.
Note
l A target altitude of 0 is considered
invalid. In the event that the radar
altimeter and radar altitude from APG-71
is not available, then the AGL altitude will
be the difference between the system
altitude and hostile area altitude (and not
the waypoint altitude).
l Entries of odd tenths will be rounded to
the next lowest even digit.
22.5.1.1 Reconnaissance Parameter Display.
Reconnaissancep arametersa re displayed on the MFl)
RECON WPT DATA 1 (Figure 22-l 1) and MFD RECON
WPT DATA 2 formats (Figure 22-12). MFD RI5
CON WPT DATA 1 format containi the reconnaissance
parameters for the fast ten waypoints. This page is selected
by depressing the R-l pushbutton on the MFD
RECON DATA statos format. The RECON WPT DATA
2 format contains the remaining ten waypoint reconnaissance
parameters. These parameters are accessed by
depressing the R-2 pushbutton on the MFD RECON
DATA statns format.
The reconnaissancep arametersc onsist of command
crossing angle, target length, map lines, and map separation
distance (map offset).
ORIGINAL 22-14
NAVAIR 0%FWAAD-1
HUD RECON SYAllBOLS
HEADING
RECON
TRACK LINE TGT BOX
STEERING
SYMBOL
CAMERA SELECTION
(SHOWN WHEN ON k____c VCN
AND RUNNING)
VDI RECON SYMBOLS
Figure 22-8. HUD/VDI ReconnaissanceS ymbology (Sheet 1 of 2)
22.15 ORIGINAL
NAVAIR 0%F14AAb1
NOMENCLATURE I FUNCTION
0 Recon Steering Symbol
0 Target Designator,
Hexagon
@
Command Ground
Track Line (CGTL)
Camera Selection
Legend
Indicates the magnetic heading for Recon steering.
- Primary steering cue for initial phase of PTP steering.
- Indicates intended magnetic heading to DSPT (as commanded by the
Recon Steering Symbol).
Provides command bank information via azimuth displacement from
velocity vector.
Displays target position referenced to the aircraft navigation system.
Displays the path of the command ground track. Indicates cross track
displacement error.
Displays the camera operational mode. First letter indicates frame position:
V=vertical, F=forward, blank=not selected.
Second letter indicates pan position: C=center, Rxight, L=left, or
blank=not selected.
Third letter indicates IRLS position: N=narrow field of view; W=wide field of
view; S=Standby; or blank=not selected.
(Note - This is only available on the HUD)
Note
When weapon is selected in A/A, the Recon Steering Symbol set
(which includes the Recon Steering Symbol; GCTL; Recon Target
Designator, and Recon Command Heading Marker) will be displayed
on the VDI
Figure 22-8. HUDMX ReconnaissanceS ymbology (Sheet2 of 2)
ORIGINAL 22.16
NAWAlR OW14AAD1
RECON
COMMAND
HEADING
MARKER
PILOT MUST FLY LEFT TO
REACH CGTL. PILOT FLlES
FLIGHT PATH MARKER TO
OVERLAP STEERING
SYMBOL. AS CORRECT
GROUND TRACK IS
REACHED, CGTL WILL
CENTER AND AIRCRAFT
WILL CROSS TARGET ON
COMMAND HEADING.
. - .
: 360 :
./. .
5L---
a 7.0
M 0.82 lOL- _ -
G 1.8
4.5
VCN
.
----J5.
<
---A,0
AIRCRAFT IS
APPROACHING
TARGET AT
COMMAND
CROSSING
ANGLE
(AT)3-F50D-313-1
Figure 22-9. HUD ReconnaissanceD isplay (Command CourseS teering)( Sheet 1 of 2)
22-l 7 ORIGINAL
NAVAlR 0%FUAAD-1
. * . .1 5- o. QR
: yo : 5L--- 4- ---J5 : 2doo:
.I* .
7,0 Q < **-
ii 0.82 lOL- - - -- -,I0
G 1.8
4.5
VCN
INITIAL APPROACH
1 SOOR * 1S OOR . * . . . .- . : 360 :
./. .
5L--- ---J5 : 2doo:
<
cl 7.0
M 0.82 IOL- - - -- -,I0
G 1.8
4.5
I I I
VCN
FOR
FINAL APPROACH
(AT)3-F50D-313-2
Figure2 2-9. HUD ReconnaissanDcies play( CommanCd ourseS teering()S hee2t of 2)
ORIGINAL 22-18
. .-- -.-. _-.
DYNAMIC
STEERING POINT
WAYPOINT 17
TARGET
TSD REPEAT
NAVAIR 01.F14AAP1
Figure 22-10. Dynamic Steering Point Display N2B7
22-19 ORIGINAL
NAVAIR 0%Fl4AAD-1
RECON R-2
RECON WPT DATA I
SMS MEN”2 ECU WPTI
Figure 22-11. h4FD RECON WPT DATA 1 Format
Figure 22-12. MFD RECON WPT DATA 2 Format
ORIGINAL 22-20
NAVAIR 0%F14AAD-1
\ I i
Xx q REPRESENTS
1 OF20 SELECTABLE
I
WAYPOINT ENTRIES
I
I I i I
I I
　
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