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

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator /

Vomaske, Richard F.
Drinkwater, Fred J.
Sadoff, Melvin
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; St...

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

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...

Flight controllability limits and related human transfer functions as determined from simulator and flight tests /

Taylor, Lawrence W.
Day, Richard E.
United States. National Aeronautics and Space Administration.

Cover title." May 1961."Aerodynamics, aircraft; Aircraft; Simulators and computers;Stability and con...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Simulator studies of simple attitude control for spin-stabilized vehicles /

Garner, H. D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Simulators and computers; Stability and control.Includes bibliographica...

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

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...

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 ...

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...

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...

Analog simulation of a pilot-controlled rendezvous /

Brissenden, Roy F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Piloting; Space mechanics; Satellites; Stability and control.Includes bibli...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator /

Vomaske, Richard F.
Drinkwater, Fred J.
Sadoff, Melvin
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; St...

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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...

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...

Flight controllability limits and related human transfer functions as determined from simulator and flight tests /

Taylor, Lawrence W.
Day, Richard E.
United States. National Aeronautics and Space Administration.

Cover title." May 1961."Aerodynamics, aircraft; Aircraft; Simulators and computers;Stability and con...

Flight investigation using variable-stability airplanes of minimum stability requirements for high-speed, high-altitude vehicles /

McFadden, Norman M.
Heinle, Donovan R.
Vomaske, Richard F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Piloting; Stability and control; Vehicle ...

Simulator studies of simple attitude control for spin-stabilized vehicles /

Garner, H. D.
United States. National Aeronautics and Space Administration.

Cover title."September 1962."Simulators and computers; Stability and control.Includes bibliographica...

Handling qualities experience with several VTOL research aircraft /

Reeder, John P.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aerodynamics, aircraft; Piloting; Stability and control; Vehicle performanc...

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...

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 ...

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...

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...

Analog simulation of a pilot-controlled rendezvous /

Brissenden, Roy F.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Piloting; Space mechanics; Satellites; Stability and control.Includes bibli...

Hovering characteristics of a rotor having an airfoil section designed for flying-crane type of helicopter /

Shivers, James P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bibl...

The effect of lateral directional control coupling on pilot control of an airplane as determined in flight and in a fixed base flight simulator /

Vomaske, Richard F.
Drinkwater, Fred J.
Sadoff, Melvin
United States. National Aeronautics and Space Administration.

Cover title."November 1961."Aerodynamics, aircraft; Aircraft; Piloting; Simulators and computers; St...

Flight-test investigation of a model of an aerial vehicle supported by four unshrouded propellers /

Kirby, Robert H.
United States. National Aeronautics and Space Administration.

Cover title."April 1962."Aerodynamics, aircraft; Aircraft; Stability and control.Includes bibliograp...

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

Abstract

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

Abstract

Extracted data

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