Influence of display and control compatibility on pilot-induced oscillations /

Airline pilot scan patterns during simulated ILS approaches /

Spady, Amos A.
Langley Research Center.

January 1978

Prepared at Langley Research Center."October 1978"--Cover.Includes bibliographical references (p. 38...

On lateral cable oscillations of cable-connected space stations /

Anderson, Willard W.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 42)....

Effect of external disturbances and data rate on the response of an automatic landing system capable of curved trajectories /

Sherman, Windsor L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Effects of activity interference on annoyance due to aircraft noise /

Willshire, Kelli F.
Powell, Clemans A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Effects of curved approach paths and advanced displays on pilot scan patterns /

Harris, Randall L.
Mixon, Randolph W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Passive control of wing/store flutter /

Reed, Wilmer H.
Foughner, Jerome T.
Cazier, F. W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Effects of combining vertical and horizontal information into a primary flight display /

Abbott, Terence S.
Nataupsky, Mark.
Steinmetz, George G.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 1...

Application of model control to wing-flutter suppression /

Ostroff, Aaron J.
Pines, Samuel.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Simulator study of a pictorial display for general aviation instrument flight /

Adams, James J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 06."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Flight-test verification of a pictorial display for general aviation instrument approach /

Adams, James J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Langley Research Center.

January 1982

"June 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

Analysis of human response in combined control tasks /

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

Prepared at Langley Research Center."March 1968"--Cover.Includes bibliographical references (p. 26)....

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"March 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Annoyance caused by propeller airplane flyover noise /

McCurdy, David A.
Powell, Clemans A.
Langley Research Center.

January 1984

Prepared at Langley Research Center."August 1984"--Cover.Includes bibliographical references (p. 35)...

Experimental study of the effects of installation on single- and counter-rotation propeller noise /

Block, P. J. W.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Airline pilot scan patterns during simulated ILS approaches /

Spady, Amos A.
Langley Research Center.

January 1978

Prepared at Langley Research Center."October 1978"--Cover.Includes bibliographical references (p. 38...

On lateral cable oscillations of cable-connected space stations /

Anderson, Willard W.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 42)....

Effect of external disturbances and data rate on the response of an automatic landing system capable of curved trajectories /

Sherman, Windsor L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Effects of activity interference on annoyance due to aircraft noise /

Willshire, Kelli F.
Powell, Clemans A.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"November 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access:...

Effects of curved approach paths and advanced displays on pilot scan patterns /

Harris, Randall L.
Mixon, Randolph W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"May 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Passive control of wing/store flutter /

Reed, Wilmer H.
Foughner, Jerome T.
Cazier, F. W.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Dec. 1980."Langley Research Center."Includes bibliographical references.Mode of access: Internet

Effects of combining vertical and horizontal information into a primary flight display /

Abbott, Terence S.
Nataupsky, Mark.
Steinmetz, George G.
Langley Research Center.

January 1987

Prepared at Langley Research Center."December 1987"--Cover.Includes bibliographical references (p. 1...

Application of model control to wing-flutter suppression /

Ostroff, Aaron J.
Pines, Samuel.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Inte...

Simulator study of a pictorial display for general aviation instrument flight /

Adams, James J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1982

Subject Category 06."March 1982"--Cover."Langley Research Center."Includes bibliographical reference...

Flight-test verification of a pictorial display for general aviation instrument approach /

Adams, James J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Langley Research Center.

January 1982

"June 1982"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: Int...

Analysis of human response in combined control tasks /

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

Prepared at Langley Research Center."March 1968"--Cover.Includes bibliographical references (p. 26)....

Operating characteristics of the Langley Mach 7 Scramjet Test Facility /

Guy, Robert W.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"March 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: In...

Annoyance caused by propeller airplane flyover noise /

McCurdy, David A.
Powell, Clemans A.
Langley Research Center.

January 1984

Prepared at Langley Research Center."August 1984"--Cover.Includes bibliographical references (p. 35)...

Experimental study of the effects of installation on single- and counter-rotation propeller noise /

Block, P. J. W.
Langley Research Center.

January 1986

Prepared at Langley Research Center."April 1986"--Cover.Includes bibliographical references (p. 8).M...

Stability and control characteristics of a three-surface advanced fighter configuration at angles of attack up to 45?/

Henderson, William P.
Leavitt, Laurence D.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"September 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access...

Airline pilot scan patterns during simulated ILS approaches /

Spady, Amos A.
Langley Research Center.

January 1978

Prepared at Langley Research Center."October 1978"--Cover.Includes bibliographical references (p. 38...

On lateral cable oscillations of cable-connected space stations /

Anderson, Willard W.
Langley Research Center.

Prepared at Langley Research Center."March 1969"--Cover.Includes bibliographical references (p. 42)....

Effect of external disturbances and data rate on the response of an automatic landing system capable of curved trajectories /

Sherman, Windsor L.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 21).Mode of ...

Influence of display and control compatibility on pilot-induced oscillations /

Abstract

Extracted data

Influence of display and control compatibility on pilot-induced oscillations /

Abstract

Extracted data

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