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| MIL-C-38418E(AS)
Mode stitch to SLAVED
Latitude control to 0
Hemisphere switch to N
Compensation switch to OFF
b.
Repeat steps b through f of 4.6.4.14.1.
c. Rotate the displacement gyroscope heading transmitter at a
rates of -6, 30, and 180 per minute.
(1)
The ac voltage from connector 2J2-8 to 2J2-9 shall
decrease to less than 0.5Vac within 30, 11, and 8 seconds, respectively.
(2)
The dc voltage from connector 2J2-17 to 2J2-18 shall
decrease to O 1Vdc within 30, 11, and 8 seconds, respectively.
(3)
The ac voltage from connector 2J2-8 to 2J2-9 shall
increase to 6.5 1Vac within 18, 26, and 35 seconds, respectively, when
the applied rates are removed.
(4)
The dc voltage from connector 2J2-17 to 2J2-18 shall
increase to a minimum of 4.0Vdc within 18, 26, and 35 seconds,
respectively, when the applied rates are removed. (The azimuth detector
input and the servoed repeater output shall be not less than 2 apart
for requirement validity.)
d.
Rotate the displacement gyroscope heading transmitter at
rates of -6, -30, and -180 per minute.
The ac voltage from connector 2J2-8 to 2J2-9 shall
(1)
decrease to less than 0.5Vac within 30, 11 and 8 seconds, repectively.
(2)
The dc voltage from connector 2J2-17 to 2J2-18 shall
decrease to O 1Vdc within 30, 11, and 8 seconds, respectively.
(3)
The ac voltage from connector 2J2-8 to 2J2-9 shall
increase to 6.5 1Vac within 18, 26, and 35 seconds, respectively, when
the applied rate is removed.
(4)
The dc voltage from connector 2J2-17 to 2J2-18 shall
increase to a minimum of 4Vdc within 18, 26, and 35 seconds,
respectively, when the applied rate is removed.
(The azimuth detector
input and the servoed repeater output shall be not less than 2 apart
for requirement validity.)
68
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