Control Systems

  • Provides control function for specific systems (Flight Control, ECS, Mission systems, etc.)
  • Collects and processes the required platform data to implement defined control function with required redundancy level (dual/triple/quadruple)
  • Produces the control outputs for defined system components (valve, actuator, motor, etc.)
  • Provides diagnostics and maintenance interfaces for development and in-service testing, diagnostics and maintenance
  • Great variety of vehicle interfaces
    • RS232, RS422, RS485, CAN, ARINC429, ARINC664/AFDX, MIL-STD-1553B, analog video, analog/discrete I/O, LVDT/RVDT inputs, DDV/RHSV, SOV outputs, power outputs, current inputs, several sensor inputs, etc.
  • Ruggedized enclosure
  • High reliability figures
  • Development lifecycle as per SAE ARP4754A
  • Qualified to MIL-STD-461, IP67, MIL-STD-810/RTCA DO-160
  • Certifiable for RTCA DO-178C and RTCA DO-254 up to Level A