Author: John F. Garren
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
VTOL Height-control Requirements in Hovering as Determined from Motion Simulation Study
Author: John F. Garren
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
VTOL Height-control Requirements in Hovering as Determined from Motion Simulator Study
Author: John F. Garren
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
VTOL Height-control Requirements in Hovering as Determined from Motion Simulation Study
Author: John F. Garren
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 15
Book Description
A Piloted Motion Simulator Investigation of VTOL Height-control Requirements
Author: Ronald M. Gerdes
Publisher:
ISBN:
Category : Flight simulators
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Flight simulators
Languages : en
Pages : 32
Book Description
Flight Investigation of V/STOL Height-control Requirements for Hovering and Low-speed Flight Under Visual Conditions
Author: James R. Kelly
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
NASA Technical Note
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 900
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 900
Book Description
Use of a Six-degrees-of-freedom Motion Simulator for VTOL Hovering Tasks
Author: Emmett B. Fry
Publisher:
ISBN:
Category : Flight simulators
Languages : en
Pages : 36
Book Description
Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristics.
Publisher:
ISBN:
Category : Flight simulators
Languages : en
Pages : 36
Book Description
Evaluation of six degrees of freedom motion simulator for Bell X-14A aircraft hovering characteristics.
A Preliminary Piloted Simulator and Flight Study of Height Control Requirements for VTOL Aircraft
Author: Ronald M. Gerdes
Publisher:
ISBN:
Category : Aircraft
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category : Aircraft
Languages : en
Pages : 24
Book Description
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1556
Book Description
A Study of Conventional Airplane Handling Qualities Requirements
Author: I. L. Ashkenas
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 86
Book Description
The report uses as a point of departure the concept that control of bank angle is the primary piloting task in maintaining or changing heading. Regulation of the bank angle to maintain heading is a close-loop tracking task in which the pilot applies aileron control as a function of observed bank angle error. For large heading changes, the steady-state bank angle consistent with available or desired load factor is attained in an open-loop fashion; it is then regulated in a closed-loop fashion throughout the remainder of the turn. For the transient entry and exit from the turn, the pilot is not concerned with bank angle per se, but rather with attaining a mentally commanded bank angle with tolerable accuracy in a reasonable time, and with an easily learned and comfortable program of aileron movements.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 86
Book Description
The report uses as a point of departure the concept that control of bank angle is the primary piloting task in maintaining or changing heading. Regulation of the bank angle to maintain heading is a close-loop tracking task in which the pilot applies aileron control as a function of observed bank angle error. For large heading changes, the steady-state bank angle consistent with available or desired load factor is attained in an open-loop fashion; it is then regulated in a closed-loop fashion throughout the remainder of the turn. For the transient entry and exit from the turn, the pilot is not concerned with bank angle per se, but rather with attaining a mentally commanded bank angle with tolerable accuracy in a reasonable time, and with an easily learned and comfortable program of aileron movements.