曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

FORMATS
The reconnaissancdei splay symbologyprovides sensor
status/ reconnaissances teering selection (via the
MFD RECON DATA status page) and the steering cues
(via HuDivDI displays) to the flightcrew. In addition,
22-9 ORIGINAL
NAVAIR OI-FMAAD-I
the position of the dynamic steering point can be displayed
on the horizontal situation display or tactical
information display/repeat on the MFD.
The MPD RECON DATA status format is selected
from the MPD MENU2 format (Figure 22-4) by depressing
the RECON pushbutton.
22.4.1 MFD RECON DATA Status Format. This
h&D format (Figure 22-S) provides the following
functions:
I. Selection of waypoint to be reconnoitered (via
increment/decrement pushtile on the upper letI
corner of the MPD RECON DATA status format)
and steering mode (point-to-point, command
course, or mapping) to be employed.
2. Displays TARPS sensor status, advisories
(TARPS and NPOV), and camera solution cues to
crew.
3. Displays target waypoint (reference point) data.
4. Provides selection of TARPS air-to-ground ranging
for AGL determination and AGL data display.
22.4.2 Reconnaissance Fault/ Problem Reportha.
The reconnaissancesv stem will reoort the TARE%
fa&.s/problems via the MPD warning, &ution, and advisory
window and store the faults in the OBC tile and
faihue. history file.
22.4.2.1 MFD Wamlng/Cautlon/Advlsory Window.
The mission computer will rcpott the following
advisories on the MFD (Figure 22-6):
1. TARPS - Reports a general failure (crew alert)
from the CPS. Monitor CPS to determine whether
or not this is a catastrophicf ailure (sensor(s)fa il).
A TARPS advisory need not scrub the reconnaisssnce
mission.
2. NPOV - Reports to the RIO that the BUS is
required to be placed in the WPOV position.
A CPZW alert is generatedfr om the CPS when
any of the following conditions occur:
a. Sensor failure (includes serial frame camera
mount position).
b. ECS failure,
c. SUDDS failure.
d. Manual VgiH in use.
e. CPS data fail (a TARP2 will be shnultaneously
stored in OBClfailure history
file).
f. Manual Vg/H test fail.
22.4.2.2 OBClFailure History File. The following
faulta will be simuhaneously stored in the OBC and
failure history tile (Figure 22-7) when the TARPS advisory
is displayed on the h4FD:
1. TARP1 - Reports a general failure (crew alert)
from the CPS.
2. TARP2 -Reports a data communication failure
between the mission computer and the CPS. This
means that the annotation data and control signals
are no longer being transmitted to TARPS.
22.4.3 Reconnaissance Steering Selection.
There are three reconnaissances teering modes available:
PTP, CCRS, and mapping. They are selected via
the MPD RECON DATA status format in either TLN,
A/G, or A/A. The steering timction is initiated when a
TARPS steering mode is selected. Steering cues will
always be computed when a steering mode is selected
and will be displayed on the BUD except in A/A with a
weapon selected. The VDI will always display steering
cues.
Before a steering mode can be selected, the waypoint
must be selected. In order to do so, the up-down arrow
on the h4PD RBCON DATA status format is used to
select the desired waypoint number. Next, by hitting
ENT, the desired waypoint parameters will be displayed.
Waypoint 17 is inhibited for reconnaissance
steering since this waypoint contains the position of the
DSPT.
22.4.3.1 Point-to-Polnt Steering. PTP is selected
when the navigation system is properly operating. Selecting
PTP ont he reconnaissancMe FD RBCON DATA
status format immediately computes the wings-level position
for the initial placement of the DSPT and computes
a heading to command the pilot to fly to that
position.
Note
The wings-level distance is approximately 4
to 8 ran from target (dependso n velocity and
altitude).
ORIGINAL 22-10
Figure 22-4. MFD MENU2 Format
Figure 22-5. MFD RECON DATA Status Format
22-11 ORIGINAL
NAVAIR 01.F14AAD-1
Figure 22-6. TARPS Advisories
In addition, the algorithm will put the reconnaissance
target designator over the target on the HUD. The PTP
steering will transition into CCRS for fmal approach
over the target.
Note
PTP remains boxed on the MFD RECON
DATA status format. The reconnaissance
steering symbol and command ground-track
line assist the pilot in a wings-level flight
over the target.
PTP steeringi s deselectedw hent he aircrafth asf lown
0.5 nm past the target or the crew manually deselects
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：F-14D 飛行手冊 Flight Manual 3(46)