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|  MIL-C-38418E(AS)
(1)
The voltage from connector 2J2-8 to 2J2-9 shall
decrease to less than 0.5Vac within 12 and 4 seconds, respectively.
(2)
The voltage from connector 2J2-17 to 2J2-18 shall
decrease to O 1Vdc within 12 and 4 seconds, respectively.
(3)
The voltage from connector 2J2-8 to 2J2-9 shall
increase to 6.5 1Vac within 8 and 14 seconds, respectively, when the
applied rate is removed.
(4)
The voltage from connector 2J2-17 to 2J2-18 shall
increase to a minimum of 4.0Vdc within 8 and 14 seconds, respectively,
when the applied rate is removed.
(The azimuth detector input and the
servoed repeater output shall be not less than 4 apart for requirement
validity.)
4.6.4.14.2.2
- Azimuth oscillations
shall be
Azimuth Oscillations
checked as follows:
a.
Set the controls on the controller and the electronic control
amplifier as follows:
Mode switch to SLAVED
Latitude control to O
Hemisphere switch to N
Compensation switch to OFF
b.
Repeat steps b through f of 4.6.4.14.2.
c.
With zero steady-state rate, drive the displacement gyroscope
transmitter to produce an azimuth oscillation of 0.8 amplitude with a
1 second period.
(1)
The voltage from connector 2J2-17 to 2J2-18 shall
at 6.5 1Vac.
connector 2J2-17 to 2J2-18 shall
(2)
The voltage
from
remain greater than 8.OVdc.
d.
Disconnect all test equipment.
4.6.4
Control Assembly Operational Tests
72
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