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198 West 21th Street, Suite 721
New York, NY 10010
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+88 (0) 101 0000 000
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Helicopter Simulation Made Easy

Fully Authority Digital Engine Control Unit

The all in-house developed Engine Control Unit (ECU) is also configurable as a Full Authority Digital Engine Control Unit (FADEC). This product, made for low-power turbojet and turboprop engines, has completed MIL-STD qualification tests, over 1,000 hours of ground testing and over 100 hours of flight tests. It is qualified according to MIL-STD-461F for EMI/EMC and with MIL-STD-810G for environmental conditions.

 

Technical Features

  • Isolated and ESD-protected interfaces (RS 422/485/232)
  • EMI/EMC compatible with MIL-STD-461F
  • Vibration and temperature resistance compatible with MIL-STD-810G
  • Operating range between -40°C and +80°C
  • In-device test and during operation test feature
  • Data recording
  • Configuration and debug modes
  • Safety modes in case of failure
    • Temperature sensor error detection
    • Speed sensor error detection
    • Open loop control mode
    • EGT hold mode
    • Transfer command standby mode