|
Collection:
|
|
NASA Dryden Flight Research Center Collection
Collection
NASA Dryden Flight Research Center Collection
Collection
|
|
Title:
|
|
F-8 DFBW pilot-induced oscillations
Title
F-8 DFBW pilot-induced oscillations
Title
|
|
Description:
|
This 28 second movie clip shows pilot induced oscillations on the F-8 DFBW aircraft. 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--confiden ce 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. F-8 DFBW Project Home Page [ http://www.nasa.gov
]
Description
This 28 second movie clip shows pilot induced oscillations on the F-8 DFBW aircraft. 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--confiden ce 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. F-8 DFBW Project Home Page [ http://www.nasa.gov
]
Description
|
|
Movie Date:
|
|
April 18, 1978
Movie_Date
April 18, 1978
Movie Date
|
|
note:
|
|
|
|
Keywords:
|
|
Langley Research Center
Keywords
Langley Research Center
Keywords
|
|
Keywords:
|
|
Dryden Flight Research Center
Keywords
Dryden Flight Research Center
Keywords
|
|
Keywords:
|
|
NASA
|
|
Keywords:
|
|
Enterprise
Keywords
Enterprise
Keywords
|
|
Keywords:
|
|
Neil Armstrong
Keywords
Neil Armstrong
Keywords
|
|
Keywords:
|
|
John Manke
Keywords
John Manke
Keywords
|
|
Keywords:
|
|
F/A-18
|
|
Keywords:
|
|
F-8
|
|
Keywords:
|
|
Digital Fly-By-Wire
Keywords
Digital Fly-By-Wire
Keywords
|
|
Keywords:
|
|
flight control
Keywords
flight control
Keywords
|
|
Keywords:
|
|
Apollo
|
|
Keywords:
|
|
Gary Krier
Keywords
Gary Krier
Keywords
|
|
Keywords:
|
|
F-16
|
|
Keywords:
|
|
space shuttles
Keywords
space shuttles
Keywords
|
|
Keywords:
|
|
pilot induced oscillation
Keywords
pilot induced oscillation
Keywords
|
|
Keywords:
|
|
Boeing 777
Keywords
Boeing 777
Keywords
|
|
facet_who:
|
|
Neil A. Armstrong
facet_who
Neil A. Armstrong
facet_who
|
|
facet_what:
|
|
WIRE
facet_what
WIRE
facet_what
|
|
facet_where:
|
|
Dryden Flight Research Center (DFRC)
facet_where
Dryden Flight Research Center (DFRC)
facet_where
|
|
facet_where:
|
|
Langley Research Center (LaRC)
facet_where
Langley Research Center (LaRC)
facet_where
|
|
facet_when:
|
|
April 18, 1978
facet_when
April 18, 1978
facet_when
|
|
facet_when_year:
|
|
1978
facet_when_year
1978
facet_when_year
|
|
Movie Number:
|
|
EM-0044-01
Movie_Number
EM-0044-01
Movie Number
|
|
UID:
|
|
SPD-DRYDEN-EM-0044-0 1
UID
SPD-DRYDEN-EM-0044-0 1
UID
|
|
original url:
|
original_url
original url
|