Special Features
2/3a c-cell gps battery installed; front connector panel: built in test; electrostatic discharge sensitive
Overall Depth
9.800 inches
Overall Height
7.000 inches
Overall Width
7.000 inches
Current Type
Dc
End Application
C/kc-135 aircraft
Mounting Method
Fixed flange
Part Name Assigned By Controlling Agency
Navigation unit, inertial-satelite signals
Voltage In Volts
28.0
Functional Description
Embedded gps/ins (egi) unit is a self-contained all-attitude navigation 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) synchronized time via externally controlled mil-std-1553b dual multiplex data bus which requests data & transmits updated data based upon the requirements of the interfacing avionics sysetems. Egi provides simultaneous ins only, blended gps/ins & gps only position solutions.
Reference Data And Literature
Dd form 61
Relationship To Similar Equipment
5 channel vs 12 channel p/n 34209200-40h4
Supplementary Features
Contains 3 ring laser gyros and 3 accelerometers in a strap down configuration, embeded global positioning system reciever
