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F-8 DFBW fin camera view of pilot-induced oscillations

Chase plane view of F-8 DFBW pilot-induced oscillations

Movie Number   EM-0044-03
Movie Date   April 18, 1978
Formats   160x120 QuickTime Movie (1.4 MB)
320x240 QuickTime Movie (2.8 MB)
480x360 QuickTime Movie (4.2 MB)
640x480 QuickTime Movie (7.0 MB)
F-8 Digital Fly-By-Wire Still photos of this aircraft are available in several resolutions at http://www.dfrc.nasa.gov/Gallery/Photo/F-8DFBW/index.html
Description  

This 38 second movie clip shows pilot-induced oscillations of the F-8 DFBW aircraft taken from a chase plane.

From 1972 to 1985 the NASA Dryden Flight Research Center conducted flight research with an F-8C employing the first digital fly-by-wire flight control system without a mechanical back up. The decision to replace all mechanical control linkages to rudder, ailerons, and other flight control surfaces was made for two reasons. First, it forced the research engineers to focus on the technology and issues that were truly critical for a production fly-by-wire aircraft. Secondly, it would give industry the confidence it needed to apply the technology--confidence it would not have had if the experimental system relied on a mechanical back up.

In the first few decades of flight, pilots had controlled aircraft through direct force--moving control sticks and rudder pedals linked to cables and pushrods that pivoted control surfaces on the wings and tails.

As engine power and speeds increased, more force was needed and hydraulically boosted controls emerged. Soon, all high-performance and large aircraft had hydraulic-mechanical flight-control systems. These conventional flight control systems restricted designers in the configuration and design of aircraft because of the need for flight stability.

As the electronic era grew in the 1960s, so did the idea of aircraft with electronic flight-control systems. Wires replacing mechanical devices would give designers greater flexibility in configuration and in the size and placement of components such as tail surfaces and wings. A fly-by-wire system also would be smaller, more reliable, and in military aircraft, much less vulnerable to battle damage. A fly-by-wire aircraft would also be much more responsive to pilot control inputs. The result would be more efficient, safer aircraft with improved performance and design.

 

Keywords   F-8; Digital Fly-By-Wire; Dryden Flight Research Center; NASA; flight control; Neil Armstrong; Apollo; Gary Krier; Langley Research Center; F-16; space shuttles; Enterprise; pilot induced oscillation; F/A-18; Boeing 777; John Manke
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