Manufactured under co-production license from Northrop Grumman Italia (NGI). The Lisa-4000 performs two distinct basic functions:

• Flight Reference.
• Navigation.

The Flight Reference function provides:

• Heading and Attitude for Display/Autopilot.
• Anti-aliasing filtered body angular rate.
• Linear Acceleration data for autopilot inner loop stability augmentation.

Navigation is performed by coupling the LISA 4000 with a Doppler Radar and Air Data Computer or with a GPS. As a navigator the LISA-4000 also outputs high speed inertial velocity data required for accurate weapon release.

The LISA-4000 therefore provides all the inertial output parameters required for Autopilot, Navigation, Display and Weapon Delivery.

General:
Size: 1/2 ATR Short/Short (322mm)
Temperature: -40^o C to +71^o C
Weight: 6.2 Kg
Cooling: Not Required
Power: 90 W, 18-32 Vdc

Outputs:
Digital ARINC-429, MIL-STD-1553B, RS-422/485 (Heading, Attitude, Accelerations, Rates, Vertical Velocity)
Synchro ARINC-407 (Heading, Pitch, Roll, Interlock for Autopilot),Eastern standard synchro output
Analog (Yaw Rate, Validities)

Accuracy

Heading: 0.8^o
Attitude: 0.5^o
Doppler/AHRS Navigation: < 1% Distance Traveled, GPS 80m CEP.

• Openess, Modularity and Scalability for a real Integration.

	CCMU-Automatic Flux Value Calibration.		DCP-Full Digital autonomous interface control.
	SBU-Eastern Avionic Integration.

	ADI/HIS-Fit & Form Cockpit retrofit with enhanced functions.		MISSION COMPUTER-In flight/on ground management of large databases, flight plans, missions.
	MAPS DISPLAYS-Several overlayed digital maps for navigation, Terrain & Obstacle Awareness.

• GPS.
• DOPPLER RADAR
• AIR DATA COMPUTER
• TACAN
• HEAD UP DISPLAY
• WEAPON DELIVERY COMPUTER
• AUTOPILOT
• VOR/ILS
• BEZO BALL