Standalone avionics PFC

Standalone avionics PFC system integrated circuits and reference designs

Description

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.

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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Technical documentation

Application notes & user guides

Application Notes (6)

Title Type Size (KB) Date
PDF 411 KB 25 Jun 2021
PDF 412 KB 29 Dec 2020
PDF 139 KB 27 Nov 2018
PDF 134 KB 23 Oct 2018
PDF 2.63 MB 23 Apr 2013
PDF 393 KB 22 Jan 2011

Product bulletin & white papers

White Papers (3)

Title Type Size (MB) Date
PDF 645 KB 20 Nov 2017
PDF 753 KB 28 Apr 2015
PDF 633 KB 24 Feb 2015

Technical articles

Support & training

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