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|  MIL-N-81604C(AS)
INDEX
(cont)
Page
Title
Paragraph
Aircraft Electrical
3.4.3.4
33
Power. . . . . . .
33
CIU Entry/Display .
3.4.3.5
Equipment Internal Interface
33
3.4.4
IMU/ANCU Interface
33
3.4.4.1
52
IMU/CAU Interface .
3.4.4.2
54
ANCU/CAU Interface
3.4.4.3
68
CIU Interface . . .
3.4.4.4
77
PSU Interface . . .
3.4.4.5
81
Detail Requirements . . . . . . . . .
3.5
81
Inertial Measuring Unit (IMU)
3.5.1
81
Function . . . . .
3.5.1.1
81
Sealing . . . . . .
3.5.1.2
Inertial Stabilized
3.5.1.3
82
Platform . . . . .
3.5.1.4
Gyro Torquing
Performance
82
Characteristics . .
Accelerometer
3.5.1.5
Quantizer Output
Performance
82
Characteristics . .
Platform
3.5.1.6
84
Electronics . . . .
84
Power Requirement .
3.5.1.7
84
Mechanical Design .
3.5.1.8
Test Equipment
3.5.1.9
90
Compatibility . . .
101
IMU Mount . . . . . . .
.
3.5.2
101
.
Function
3.5.2.1
101
Mechanical Design
.
3.5.2.2
103
Power Supply Unit (PSU) . .
.
3.5.3
103
Function . . .
.
.
3.5.3.1
103
Input Power . . .
.
3.5.3.2
104
Output Power . .
.
3.5.3.3
Battery Back-up
3.5.3.4
Power. . . . . .
.
104
106
Mechanical Design
.
3.5.3.5
197
.
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