 |
|||
|
Page Title:
Figure 3. Effect of Data Link Loss on Reaction Time |
|
||
| ||||||||||
|
|  MIL-N-81604C(AS)
Para 3.4.1.1.3a
(cont)
Carrier Alignment - This is the alignment
submode for the equipment aboard an aircraft
carrier. This mode shall be initiated by
placing the CIU MODE switch in the NORM
position while on an aircraft carrier with
valid data link information available. While
in this suhnode, the alignment sequence will
be performed automatically. The controlling
computer will receive ship's signals in
accordance with AR-57. In the event that
data link information is lost during align-
ment, the allowable reaction time, as speci-
*
fied in 3.3.11, shall be increased by an
amount equal to the total of the lost data
*
link intervals plus 20 seconds. Refer to
figure 3. Waypoint information may be re-
ceived from the data link when requested.
Figure 3. Effect of Data Link Loss on Reaction Time
23
|
|
Privacy Statement - Press Release - Copyright Information. - Contact Us |
Click
here for thousands of PDF manuals