Flight Controls

Poilot Controls

IFCS Integration

Ground Test

Pilot Controls

STICK AND PEDAL ASSEMBLY PHOTO FROM CEF

• Stick and Pedal Assembly consists of Artificial Feel Unit and Damper to suit   handling qualities requirements
• Quadruplex LVDTs from pilots command, interfaced to DFCC.

INTERFACES WITH AVIONICS SYSTEM : 

HUD and MFD Photograph from CEF

• Avionics System Interface through MIL STD 1553B Bus.
• Exchange of IFCS Failure management data on  Air data.
• Pilot Vehicle Interface for Warnings Management  through HUD and MFDs.
• User friendly dialogues for Interactive Built-in-Tests
• Interface with Centralised Warning Panel and  Get-U-Home Panel.