Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks /

Attitude control requirements for hovering determined through the use of a piloted flight simulator /

Faye, Alan E.
United States. National Aeronautics and Space Administration.

Cover title." April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; Stab...

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

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....

VTOL height-control requirements in hovering as determined from motion simulation study /

Garren, John F.
Assadourian, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft safety and noise; Simulators and computers; Stability and contro...

A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft /

Gerdes, Ronald M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aircraft; Simulators and computers; Stability and control.Includes bibli...

Effects of gyroscopic cross coupling between pitch and roll on the handling qualities of VTOL aircraft /

Garren, John F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Simulators and computers;Stability and control;Vehicle performance;Includes...

A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle /

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; Simula...

Transition and hovering flight characteristics of a tilt-duct VTOL research aircraft /

Kelley, Henry L.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks

Greif, R. K.
Gerdes, R. D. M.
Fry, E. B.

August 1969

Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristi...

A simulator and flight study of yaw coupling in turning maneuvers of large transport aircraft /

McNeill, Walter E.
Innis, Robert C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (19-20).Mode of access: Internet

Simulation studies for planning an in-flight experiment to define manual guidance and control techniques for large launch vehicles /

Watson, DeLamar M.
Stinnett, Glen W.
Hardy, Gordon H.
Ames Research Center.

Prepared at Ames Research Center."April 1969"--Cover.Includes bibliographical references (p. 26).Mod...

Attitude control requirements for hovering determined through the use of a piloted flight simulator /

Faye, Alan E.
United States. National Aeronautics and Space Administration.

Cover title." April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; Stab...

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

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....

VTOL height-control requirements in hovering as determined from motion simulation study /

Garren, John F.
Assadourian, Arthur.
United States. National Aeronautics and Space Administration.

Cover title."October 1962."Aircraft safety and noise; Simulators and computers; Stability and contro...

A preliminary piloted simulator and flight study of height control requirements for VTOL aircraft /

Gerdes, Ronald M.
United States. National Aeronautics and Space Administration.

Cover title."February 1962."Aircraft; Simulators and computers; Stability and control.Includes bibli...

Effects of gyroscopic cross coupling between pitch and roll on the handling qualities of VTOL aircraft /

Garren, John F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Simulators and computers;Stability and control;Vehicle performance;Includes...

A flight determination of the attitude control power and damping requirements for a visual hovering task in variable stability and control X-14A research vehicle /

Rolls, L. Stewart.
Drinkwater, Fred J.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Aircraft safety and noise; Piloting; Simula...

Transition and hovering flight characteristics of a tilt-duct VTOL research aircraft /

Kelley, Henry L.
United States. National Aeronautics and Space Administration.

Cover title."November 1962."Includes bibliographical references.Mode of access: Internet

Flight investigation of the longitudinal stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Force-test investigation of the stability and control characteristics of a four-propeller tilt-wing VTOL model with a programed flap /

Newsom, William A.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes biblio...

Force-test investigation of the stability and control characteristics of a 1/8-scale model of a tilt-wing Vertical-Take-Off-and-Landing (VTOL) airplane /

Tosti, Louis P.
Langley Research Center.

January 1960

"NASA TN D-44.""Langley Research Center, Langley Field, Va.""March 1960."Title from cover.Includes b...

Hovering and transition flight tests of a 1/5-scale model of a jet-powered vertical-attitude VTOL research airplane /

Smith, Charles C.
United States. National Aeronautics and Space Administration.

Cover title."May 1961."Aerodynamics, aircraft; Aircraft;Includes bibliographical references.Mode of ...

Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks

Greif, R. K.
Gerdes, R. D. M.
Fry, E. B.

August 1969

Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristi...

A simulator and flight study of yaw coupling in turning maneuvers of large transport aircraft /

McNeill, Walter E.
Innis, Robert C.
Ames Research Center.
United States. National Aeronautics and Space Administration.

January 1967

Cover title."May 1967."Includes bibliographical references (19-20).Mode of access: Internet

Simulation studies for planning an in-flight experiment to define manual guidance and control techniques for large launch vehicles /

Watson, DeLamar M.
Stinnett, Glen W.
Hardy, Gordon H.
Ames Research Center.

Prepared at Ames Research Center."April 1969"--Cover.Includes bibliographical references (p. 26).Mod...

Attitude control requirements for hovering determined through the use of a piloted flight simulator /

Faye, Alan E.
United States. National Aeronautics and Space Administration.

Cover title." April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; Stab...

Flight-test evaluation of STOL control and flight director concepts in a powered-lift aircraft flying curved decelerating approaches /

Hindson, W. S.
Innis, Robert C.
Hardy, Gordon H.
Ames Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"March 1981"--Cover."Ames Research Center."Includes bibliographical references.Mode of access: Inter...

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....

Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks /

Abstract

Extracted data

Use of a six-degrees-of-freedom motion simulator for VTOL hovering tasks /

Abstract

Extracted data

Related items

Related items