Aircraft flight control system

A typical aircraft's primary flight controls in motion

A conventional fixed-wing aircraft flight control system (AFCS) consists of flight control surfaces, the respective cockpit controls, connecting linkages, and the necessary operating mechanisms to control an aircraft's direction in flight. Aircraft engine controls are also considered flight controls as they change speed.

The fundamentals of aircraft controls are explained in flight dynamics. This article centers on the operating mechanisms of the flight controls. The basic system in use on aircraft first appeared in a readily recognizable form as early as April 1908, on Louis Blériot's Blériot VIII pioneer-era monoplane design.[1]

  1. ^ Crouch, Tom (1982). Blériot XI, The Story of a Classic Aircraft. Smithsonian Institution Press. pp. 21 & 22. ISBN 978-0-87474-345-6.