DISPLAY SYSTEM

    • Multi-Functional Display (MFD)

      • Multi-Function Display (MFD) provides the pilot with high resolution symbology overlaid on a video image coming from DMG and other interface systems. The MFD is built around a full high resolution, high contrast Active Matrix Liquid Crystal Display (AMLCD) device, allowing pilot to see the display image even under a high ambient light. It has high MTBF, 4 times in comparison to CRT. It displays video images coming from video sources such as RADAR, FLIR, OPTRONICS and Digital Map Generator.

    • Pilot Control Unit (PCU) for Helicopters

      • Pilot Control Unit (PCU-II) is Human Machine Interface (HMI) of Automatic Flight Control System (AFCS). It provides interface between crew and AFCS.

    • Engine & Flight Display Unit (EFDU)

      • Engine & Flight Display Unit (EFDU) is LCD display for EFIS system. It displays Air Data, Attitude, Heading information, Engine, fuel and hydraulic parameters information. EFIS is also integrated with avionics system through MIL 1553B bus.

    • Head Up Display System (HUD)

      • Head Up Display (HUD) system is designed to display aircraft symbology in various modes to the pilot. The aircraft symbology is displayed through a combiner lens assembly which displays the symbology superimposed on the external field of view.

    • Combined Map and Electronic Display (COMED)

      • The Head down display (Combined Map and Electronic Display, COMED-2045) is a cockpit mounted navigational aid with multifunction facilities. It displays the ground map as stored in a filmstrip superimposed with symbols generated in a CRT. The projected map corresponds to the terrain over which the aircraft is flying in the navigational mode. The CRT displays the symbols corresponding to the present position, heading of the aircraft track and direction to the next waypoint. The CRT also provides various other flight parameters such as altitude, air speed, ground speed, time to go to next waypoint etc. Facilities are also available to project flight instrument parameters. The equipment is integrated to the Navigation/Attack system through MIL-STD -1553B bus.

    • Head Up Display and Weapon Aiming Computer (HUDWAC)

      • The Head Up Display and weapon aiming computer, HUDWAC provides the pilot with continuously updated weapon-aiming information accurately superimposed on his forward view of the outside world. The system generates and positions aiming marks and other symbols in a range of attack mode, using data provided by the Inertial Navigation and Attack system (INS) through the MIL-STD-1553B bus.

    • Helmet Mounted Display System

      • Helmet Mounted Display System  is meant for determination of angular co-ordinates of visually observable target, as per movement of pilot head.

    • SYSTEM PANEL

      • System panel is intended for data reception, entry, processing and display of information as well as for selection of mode.

    • Avionics Division Korwa

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