Special Features:

A) provides outputs of: acceleration, velocity, position, heading, attitude, attitude rates (roll, pitch, azimuth) b) contains 3 ring laser gyros and 3 accelerometers in a strapdown configuration c) embedded global positioning system receiver (egr) (rf input)- gasr based d) 1553/b multiplex bus compatible e) built in test incorporated f) 32 bit microprocessor g) arinc 429 interface card h) multi-mode receiver that provides: instrument landing system (ils), very high omni bearing receiver (vor), marker beacon (mb).

Properties:

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 unit(s);platform, inertial; power supplies; subsystems; mode selectors; and control displays.