Standalone avionics PFC

Products and reference designs

Standalone avionics PFC

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Overview

Our integrated circuits and reference designs help you develop highly-efficient standalone avionics precision flight control (PFC) solutions to meet the DO-160 and MIL-STD-810 standards while also reducing size and weight.

Design requirements:

Modern standalone avionics PFC systems require:

  • Meeting DO-160 THD and EMI specifications.
  • Reducing size and weight of system components to maximize aircraft fuel efficiency.
  • Support for variable (360Hz to 800Hz) frequency AC power.

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