Add to ORKGThe utility of a visual display when studying the influence of changes in lateral stick gearing gains on the Highly Maneuverable Aircraft Technology (HiMAT) vehicle handling qualities during simulated approaches and landings is investigated. The visual display improved the validity of the simulation and provided improved roll response cues for the HiMAT aircraft landing approach. A range of acceptable constant lateral stick gearing gains is found that provides adequate maneuverability and allows for precision moments
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A six degree of freedom, fixed base simulation study of the use of a flight director by general avia...
Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicle
A simulator evaluation of a remotely piloted research vehicle was conducted at NASA Ames Research Ce...
Tests were conducted to determine the significance of vertical acceleration cues in the simulation o...
Preliminary tests and evaluation are presented of pilot performance during landing (flight paths) us...
The essential features of using pitch attitude for glidepath control in conjunction with longitudina...
Report presents the results of studies made in an attempt to provide information on the control oper...
A computer drawn instrument landing approach display, which shows a box located on the desired path,...
A computerized analysis procedure, based on a control theoretic model of the human pilot, is used to...
The flight simulation facility features an extensive cockpit motion system, emphasizing lateral moti...
Developing lateral stability and directional control handling qualities in landing approach control ...
The optimal control model (OCM) of the human operator is used to predict the effect of simulator cha...
A head-up general aviation landing aid called a landing site indicator (LASI) was tested in a fixed-...
This paper describes a piloted simulation conducted on the NASA Ames Vertical Motion Simulator. The ...
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A six degree of freedom, fixed base simulation study of the use of a flight director by general avia...
Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicle
A simulator evaluation of a remotely piloted research vehicle was conducted at NASA Ames Research Ce...
Tests were conducted to determine the significance of vertical acceleration cues in the simulation o...
Preliminary tests and evaluation are presented of pilot performance during landing (flight paths) us...
The essential features of using pitch attitude for glidepath control in conjunction with longitudina...
Report presents the results of studies made in an attempt to provide information on the control oper...
A computer drawn instrument landing approach display, which shows a box located on the desired path,...
A computerized analysis procedure, based on a control theoretic model of the human pilot, is used to...
The flight simulation facility features an extensive cockpit motion system, emphasizing lateral moti...
Developing lateral stability and directional control handling qualities in landing approach control ...
The optimal control model (OCM) of the human operator is used to predict the effect of simulator cha...
A head-up general aviation landing aid called a landing site indicator (LASI) was tested in a fixed-...
This paper describes a piloted simulation conducted on the NASA Ames Vertical Motion Simulator. The ...
The simulation employed all six rigid-body degrees of freedom and incorporated aerodynamic character...
A six degree of freedom, fixed base simulation study of the use of a flight director by general avia...
Flight simulator to evaluate lateral-directional handling qualities of piloted reentry vehicle