Hardware-in-the-Loop (HIL) flight control validation, multi-channel strain and pressure instrumentation, and deterministic data logging supporting ARINC 429, MIL-STD-1553, and Ethernet TSN pipelines with sub-microsecond synchronization.
Rigorous flight actuator testing requires simultaneous phase-locked acquisition of pressure dynamics, displacement LVDTs, strain foil bridges, and tri-axial acceleration. Our modular DAQ frontend provides simultaneous sampling across all channels at up to 100 kS/s per channel with IEEE 1588 PTP sub-microsecond time-stamping.
Engineered inside a conduction-cooled, sealed aluminum enclosure with heavy-duty circular MIL-DTL connectors. Employs multi-core ARM Cortex-A + dedicated FPGA fabric to execute real-time frequency-response function (FRF) calculations, modal damping estimation, and limit checking in under 50 microseconds.
Directly sniffs and decodes command words from aircraft avionics buses while correlating flight control computer (FCC) commands with physical hydraulic pressures and actuator position feedback. Bridges flight-bus telemetry smoothly to Time-Sensitive Networking (TSN) and Gigabit Ethernet uplinks.
Integrated high-speed NVMe solid-state storage logs uncompressed continuous raw time-series data throughout full endurance qualification cycles (10,000+ flight hours). Seamlessly integrates into MATLAB/Simulink, LabVIEW, and custom Python aerodynamic models via ultra-low-latency gRPC and shared memory buffers.
Consult with our avionics instrumentation and FPGA DSP hardware engineers.
