Special Features
Additional information computed: climb angle, vertical velocity, ground speed to altitude ratio
Mounting Type
Base, shock mount
End Application
An/asn-56 inertial navigation sys; rf4c aircraft
Unpackaged Unit Length
23.600 inches
Unpackaged Unit Width
4.250 inches
Unpackaged Unit Height
9.740 inches
Power Source
External
Input Intelligence Type
Altitude, general data and ground speed and pitch-roll signal data
Intelligence Input Method
Electrical
Output Intelligence Type
Angle of attack
Functional Description
Contains the follow-up servos for pitch and roll information from the inertial navigation set stable platform, and circuitry for computing vertical attack angle, climb angle, vertical velocity, and ground speed to altitde ratio
