Inertial Navigation System

Model / MPN: CN-1689(V)16/ASN | NSN: 6605-01-532-6515

A self-contained, dead-reckoning system that senses acceleration along the pitch, yaw and roll axis of the aircraft and calculates the distance traveled from a reference point. They can include inertial navigation uni (s) ; platform, inertial; power supplies; subsystems; mode selectors; and control displays.

Product Details

NATO Stock Number

6605-01-532-6515

Sold in multiples of

1 EA

DEMIL

DEMIL/MLI

Overall Height

11.000 inches

Overall Width

8.500 inches

End Application

Cn-1689

Functional Description

The p3i embedded gps/ins (egi)+ with multi mode receiver (mmr) unit is a self- contained all attitude navagation line replaceable unit providing outputs of acceleration, attitude (azimuth, pitch, roll), attitude rates, heading, position, velocity, associated time tag information, and universal time coordinated (utc) sychronized time via externally controlled mil-std-1553b dual multiplex data bus which receives data and transmits updated data based the requirements of the interfacing avionics systems. The mmr provides for a protected instrument landing system (p-ils), a very high omni bearing receiver (vor), and a marker beacon (mb) functionality. The egi+ w/mmr provides simultaneous inertial, blended and gps only position solutions. It incorporates a gsar based receiver.

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CN-1689(V)16/ASN Cross Reference

34249950-R004-960