Effects of high sustained acceleration on pilots' performance and dynamic response /

Measured transfer functions of pilots during two-axis tasks with motion /

Bergeron, Hugh P.
Adams, James J.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Includes bibliographical references (p. 9).M...

Development and flight test of an experimental maneuver autopilot for a highly maneuverable aircraft /

Duke, Eugene L.
Roncoli, Ralph B.
Jones, Frank P.
Ames Research Center.

January 1986

Prepared at Ames Research Center."September 1986"--Cover.Includes bibliographical references (p. 30)...

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Effects of flight simulator motion of pilots' performance of tracking tasks /

Douvillier, Joseph G.
Ames Research Center.

Prepared at Ames Research Center."February 1960."Cover title.Includes bibliographical references (p....

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Rough-air effect on crew performance during a simulated low-altitude high-speed surveillance mission /

Hurt, George J.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

Human pilots' dynamic response characteristics measured in flight and on a nonmoving simulator /

Kuehnel, Helmut A.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Behavioral studies; Piloting; Simulators and comput...

High altitude gust acceleration environment as experienced by a supersonic airplane /

Ehernberger, L. J.
Love, Betty J.
Flight Research Center (U.S.)

January 1975

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 23-24).M...

Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack /

Larson, Terry J.
Ames Research Center.

Prepared at Ames Research Center."April 1987"--Cover.Includes bibliographical references (p. 22-23)....

Study of dynamic response to impact loadings of acceleration sensors having various mounting characteristics /

McCarty, John Locke.
Pearson, Jerome.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

The effects of motion and g-seat cues on pilot simulator performance of three piloting tasks /

Showalter, Thomas W.
Parris, Benton L.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Int...

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

Prepared at Langley Research Center."April 1960."Cover title.Includes bibliographical references (p....

A simulation investigation of the loads experienced by a piloted launch vehicle /

Sleeper, Robert K.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 33)....

Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet /

Cole, Henry A. Jr.
Holleman, Euclid C., joint author.
Brown, Stuart C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "November 26, 1954."Includes bibliographical references: p. 32-33.Mode of access: In...

Effects of peak deceleration on range sensitivity for a modulated-lift reentry at supercircular speeds /

Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."September 1963."Includes bibliographical references.Mode of access: Internet

Measured transfer functions of pilots during two-axis tasks with motion /

Bergeron, Hugh P.
Adams, James J.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Includes bibliographical references (p. 9).M...

Development and flight test of an experimental maneuver autopilot for a highly maneuverable aircraft /

Duke, Eugene L.
Roncoli, Ralph B.
Jones, Frank P.
Ames Research Center.

January 1986

Prepared at Ames Research Center."September 1986"--Cover.Includes bibliographical references (p. 30)...

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Effects of flight simulator motion of pilots' performance of tracking tasks /

Douvillier, Joseph G.
Ames Research Center.

Prepared at Ames Research Center."February 1960."Cover title.Includes bibliographical references (p....

Jet effects at supersonic speeds on base and afterbody pressures of a missile model having single and multiple jets /

Charczenko, Nickolai.
Hayes, Clyde.
Langley Research Center.

Prepared at Langley Research Center."November 1963"--Cover.Includes bibliographical references (p. 8...

Rough-air effect on crew performance during a simulated low-altitude high-speed surveillance mission /

Hurt, George J.
Langley Research Center.

Prepared at Langley Research Center."August 1963."Cover title.Includes bibliographical references (p...

Human pilots' dynamic response characteristics measured in flight and on a nonmoving simulator /

Kuehnel, Helmut A.
United States. National Aeronautics and Space Administration.

Cover title."March 1962."Aerodynamics, aircraft; Behavioral studies; Piloting; Simulators and comput...

High altitude gust acceleration environment as experienced by a supersonic airplane /

Ehernberger, L. J.
Love, Betty J.
Flight Research Center (U.S.)

January 1975

Prepared at NASA Flight Research Center.Cover title.Includes bibliographical references (p. 23-24).M...

Qualitative evaluation of a flush air data system at transonic speeds and high angles of attack /

Larson, Terry J.
Ames Research Center.

Prepared at Ames Research Center."April 1987"--Cover.Includes bibliographical references (p. 22-23)....

Study of dynamic response to impact loadings of acceleration sensors having various mounting characteristics /

McCarty, John Locke.
Pearson, Jerome.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (p. 16).Mode of access: Internet

The effects of motion and g-seat cues on pilot simulator performance of three piloting tasks /

Showalter, Thomas W.
Parris, Benton L.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"January 1980"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Int...

Fixed-base simulation study of a pilot's ability to control a winged-satellite vehicle during high-drag variable-lift entries /

Eggleston, John M. (John Marshall)
Cheatham, Donald C.
Baron, Sheldon.
Langley Research Center.

Prepared at Langley Research Center."April 1960."Cover title.Includes bibliographical references (p....

A simulation investigation of the loads experienced by a piloted launch vehicle /

Sleeper, Robert K.
Langley Research Center.

Prepared at Langley Research Center."March 1966"--Cover.Includes bibliographical references (p. 33)....

Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet /

Cole, Henry A. Jr.
Holleman, Euclid C., joint author.
Brown, Stuart C., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "November 26, 1954."Includes bibliographical references: p. 32-33.Mode of access: In...

Effects of peak deceleration on range sensitivity for a modulated-lift reentry at supercircular speeds /

Jackson, Charlie M.
Harris, Roy V.
United States. National Aeronautics and Space Administration.

Cover title."September 1963."Includes bibliographical references.Mode of access: Internet

Measured transfer functions of pilots during two-axis tasks with motion /

Bergeron, Hugh P.
Adams, James J.
Langley Research Center.

Prepared at Langley Research Center."March 1964"--Cover.Includes bibliographical references (p. 9).M...

Development and flight test of an experimental maneuver autopilot for a highly maneuverable aircraft /

Duke, Eugene L.
Roncoli, Ralph B.
Jones, Frank P.
Ames Research Center.

January 1986

Prepared at Ames Research Center."September 1986"--Cover.Includes bibliographical references (p. 30)...

Effects of simulated rocket-jet exhaust on stability and control of a research-type airplane configuration at mach number of 6.86 /

Fetterman, David E.
United States. National Aeronautics and Space Administration.

"October 1959."Cover title.Includes bibliographical references (p. 15).Mode of access: Internet

Effects of high sustained acceleration on pilots' performance and dynamic response /

Abstract

Extracted data

Effects of high sustained acceleration on pilots' performance and dynamic response /

Abstract

Extracted data

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