Data acquisition unit for flight test instrumentation

Data Acquisition Units (DAUs)

  • Configurable chassis with multiple I/O boards in order to drive the required sensors (e.g., IMUs, accelerometers, Pitot tubes, etc..) and databus formats (e.g., ARINC‑429, MIL‑STD‑1553, Ethernet, AFDX, RS‑232/422, etc.).
  • Multiplexes multi‑sensor inputs into a unified output stream.
  • Onboard sensor management: power, data conditioning, and health checks.
  • Scalable from single DAU to multi‑node FTI networks.
  • Designed for shock/vibration profiles in demanding flight tests.

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