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Page Title:
Table 111. ASK-32/A24G-39 or ASK-44/A24G Electronic Control Amplifier Connector to Displacement Gyroscope |
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|  MIL-C-38418E(AS)
Provisions shall be made for the excitation of the magnetic
and VI.
azimuth detector, DSU-4A/A, conforming to MIL-D-38134, or the ML-1
connforming to MIL-T-19576.
ASK-32/A24G-39 or ASK-44/A24G Electronic
TABLE 111.
Control Amplifier Connector to Displacement
Gyroscope
Function
Pins
Azimuth input
1 (S1)
Azimuth input
2 (S2)
Azimuth input
3 (S3)
Erection warning
4
Linear acceleration signal
5
Not used
6
Pitch control
7
Roll control
8
Ground (neutral)
9
115V A
10
115V B
11
115V C
12
Fast erection control excitation, 78V C
13
Spare
14
Spare
15
Spare
16
N. latitude control and slating
17
S. latitude control and slating
18
Pitch input
19 (S1)
Pitch input
20 (S2)
Pitch input
21 (S3)
Roll input
22 (S1)
Roll input
23 (S2)
Roll input
24 (S3)
1/ Connector (2J2) MS24264R16B24S6X to mate with
MS24266R16B24P6
14
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