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File:F-8C FBW.jpg

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Text and image from nasa.gov:

F-8C Digital-Fly-By-Wire Control System was first tested in 1972. The use of electrical and mechanical systems to replace hydraulic systems for aircraft control surface actuation was flight-tested. Today widely used by commercial airliners, the Digital-Fly-By-Wire Control System allows for better maneuver control, smoother rides, and for military aircraft, a higher combat survivability. For more information please read James Tomayko’s book Computers Take Flight:A History of NASA's Pioneering Digital Fly-By-Wire Project (NASA SP-2000-4224), which can be found here.

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current06:31, 6 March 2007Thumbnail for version as of 06:31, 6 March 2007738 × 432 (198 KB)Admin (talk | contribs)Text and image from nasa.gov: F-8C Digital-Fly-By-Wire Control System was first tested in 1972. The use of electrical and mechanical systems to replace hydraulic systems for aircraft control surface actuation was flight-tested. Today widely used by commercial airliners, the Digital-Fly-By-Wire Control System allows for better maneuver control, smoother rides, and for military aircraft, a higher combat survivability. For more information please read James Tomayko’s book Computers Take Flight:A History of NASA's Pioneering Digital Fly-By-Wire Project (NASA SP-2000-4224), which can be found [http://www.dfrc.nasa.gov/History/Publications/f8ctf here]. {{PD-USGov-NASA}}
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