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| MIL-C-38418E(AS)
d.
Set the indicated heading of output No. 1 to 0 as
tabulated, using the simulated displacement gyroscope heading transmitter.
e.
Adjust the 0 compensation potentiometer on the electronic
control amplifier to produce a null voltage from connector 2J2-17 to
2J2-18 as follows:
ASK-32/A24G-39
O 0.5 Vdc
ASK-44/A24G
O 0.25 Vdc
f.
Repeat steps c, d, and e for each of the table XX tabulated
heading pairs, in sequence.
TABLE XX.
Heading Scale Error Tabulation
Azimuth Detector Heading
Indicated Heading
0 23'
0
16 09'
15
31 49'
30
47 23'
45
62 46'
60
75
77 58'
92 58'
90
107 46'
105
122 23'
120
136 49'
135
151 09'
15o
165 23'
165
179 37'
180
193 51'
195
208 11'
210
222 37'
225
237 14'
240
252 02'
255
267 02'
270
282 14'
285
297 37'
300
313 11'
315
328 51'
330
344 37'
345
60
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