Avionics: Flight Control System



The flight control systems of modern day aircraft vary with the size and performance expected by the aircraft. Fly-by-wire (FBW) or digital fly-by-wire (DFBW) are replacing the traditionally mechanical or hydraulic systems of the past. Sensor measurements around the plane (gyros, air speed sensors, etc.) are combined with pilot commands from the cockpit to deliver commands to various actuators located at each of the aircraft’s control surfaces. TI has developed products and design resources in order to meet the high demands of flight control systems. These include:

  • Solutions featuring TI’s Enhanced Product (EP) portfolio, which allows designs to meet the extreme temperature fluctuations with -55 to 125°C rated products
  • Industrial grade Ethernet PHYs for use in protocols such as AFDX/ARINC 664
  • EXT power modules that have been tested to meet the vibration and drop standards MIL-STD-883 Method 2007.2 and Method 2002.3, respectively
  • Resolver-to-digital converters (RDCs) for a highly integrated solution for controlling the slats and flaps in the harsh conditions found on the edge of the aircraft’s wings

Selection & solution guides

Selection Guides (1)

Title Abstract Type Size (KB) Date Views
PDF 5.75 MB 19 Aug 2016 5391

Solution Guides (3)

Title Abstract Type Size (KB) Date Views
PDF 790 KB 21 May 2015 2433
PDF 1.24 MB 19 Mar 2015 2440
PDF 2.65 MB 14 Jan 2014 3464

Product bulletin & white papers

White Papers (2)

Title Abstract Type Size (MB) Date Views
PDF 881 KB 15 Jun 2016 283
PDF 1.02 MB 05 Apr 2016 3244

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