Flight Control Systems and Computers
Enhancing flight safety, performance, and reliability with cutting-edge Fly-by-Wire (FBW) technology for aircraft, helicopters, and eVTOLs.
Thales' expertise in Fly-by-Wire (FBW) spans over 40 years and 12,000 aircraft. From the early days of the Airbus A320 airliner to the latest Gulfstream G800, Thales has been at the forefront of FBW innovation. By providing aircraft manufacturers with solutions ranging from single-axis or secondary flight control computers and electronics to complete integration of flight control systems. Thales has grown to become one of the largest flight control electronics system supplier in the world.
FORCES
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40+ Years of Leadership
Thales pioneered Fly-by-Wire (FBW) tech from the Airbus A310 to today’s most advanced aircraft. With 12,000+ platforms equipped and global certifications, Thales ensures unmatched reliability, safety, and in-service support across aviation sectors.
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Smart & Scalable Systems
From full FBW shipsets to Smart Electronic Control Units (SECU) and Remote Electronic Units (REU), Thales offers modular, high-integrity systems. These solutions meet the needs of all aircraft types—jets, helicopters, eVTOLs—with ease of integration.
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Fast Cert & Update Tools
Thales' unique design and certification tools support real-time flight test tuning and automated code generation. This drastically reduces development time and cost, enabling faster certification and in-field software updates for operators.
Thales Flight Control Systems on board major programs
Thales pioneered the development and certification of FBW technology on modern aircraft, starting with the Airbus wide-body A310 in 1983 followed by the A320 family where Thales supplies the Spoiler Elevator Computer (SEC), Elevator Aileron Computer (ELAC), and Flight Augmentation Computer (FAC). Thales also supplies full flight control systems on the Bombardier CRJ 700/900/1000 and Global 5000/6000 aircraft families.
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The Flight Control Computer (FCC) is a high integrity, low SWaP (Size, Weight and Power) airborne computer that comprises two channels operating in an active/standby configuration. Each channel directly performs the inceptor position acquisition via analog sensors, processes the aircraft manufacturer control laws, and provides digital commands to control the flight control surfaces. It also consolidates and reports the statuses of all flight control system equipment for annunciation to the flight and maintenance crews. The FCC manages the various system modes as well as the active/standby redundancy between both channels of the same FCC.
FEATURES
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KEY FIGURES