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SYSTEM DESCRIPTION, INSTALLATION, AND MAINTENANCE MANUAL
B. System Status Reports
45D25'12.8"N
74D51'8.8"W
CHAN
C/N0
SIG dB
1
****
*****
19:26:15 DOP=-50
LOOK ANGLE=33.1
45D25'12.8"N
74D51'8.8"W
CHAN
C/N0
SIG dB
1
****
*****
19:26:16 DOP=-50
LOOK ANGLE=33.1
Output Example
45D25'12.8"N 74D51'8.8"W
PT 0.2D
RL 0.0D
HD 79.8D
TK 0.2D
40 knots
150 ft
19:26:15
DOP=-50
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Aspire-200
3. To navigate through the list of reports, press CTRL + N.
4. To access a report, type the number next to the report name, and then press
ENTER.
The vt100 scenario report provides information about various aspects of the channel
card operation.
To view the report, in the list of available reports, press the number next to vt100
scenario report.
Figure 6-1 provides an example of the output of the report.
PT 0.2D
RL 0.0D
TEMP
BEAM
STAT
????
?
booting
PT 0.2D
RL 0.0D
TEMP
BEAM
STAT
????
?
booting
Figure 6-1 VT100 Scenario Report
Table 6-1 provides descriptions of the items in the report.
Table 6-1 VT100 Scenario Report Content
IRS latitude and longitude position as interpreted by the HDU
Aircraft pitch angle, where nose UP is positive
Aircraft roll angle, where cw is positive
Aircraft true heading; where the nose of the aircraft is pointingin
reference to True North
Aircraft true track; direction the aircraft is traveling—not
necessarily the direction it is heading
Aircraft velocity—may display **** when the aircraft is on the
ground, depending on the navigation source.
Altitude
Time based on the system real time clock
Doppler frequency offset
HD 79.8D
TK 0.2D
40 knots
BT
OC
TX
dBW
58
NO
0.000
0.0
HD 79.8D
TK 0.2D
40 knots
BT
OC
TX
dBW
58
NO
0.000
0.0
Description
23-15-45
150 ft
WATT
0
150 ft
WATT
0
Page 6-4
4 Dec 2015
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